Started by upstream project "ESP_Beta" build number 710
originally caused by:
 Started by remote host 18.18.33.14
Running as SYSTEM
[EnvInject] - Loading node environment variables.
Building remotely on reynolds-centOS8 in workspace /home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64
Cleaning local Directory .
Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-04-27T17:47:59.928 -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 2480

Checking out a fresh workspace because /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/JenkinsESP doesn't exist
Cleaning local Directory JenkinsESP
Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-04-27T17:47:59.928 -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 857

No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
No changes for svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP since the previous build
[GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[Execution node] check if [reynolds-centOS8] 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/jenkins15329779880973617027.sh
+ bash -ex /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/JenkinsESP/ESP_Beta.sh
+ source /home/jenkins/workspace/ESP_Beta/7.7/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=3.11.6
++ PYTHON_VERSION=3.11.6
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ reynolds-centOS8 == \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
++++ '[' -z '' ']'
++++ BASHRCSOURCED=Y
++++ '[' '' ']'
++++ 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/bash_completion.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/bash_completion.sh
+++++ '[' -n '4.4.20(1)-release' -a -n '' -a -z '' ']'
++++ 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/colorxzgrep.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/colorxzgrep.sh
+++++ /usr/libexec/grepconf.sh -c
+++++ alias 'xzgrep=xzgrep --color=auto'
+++++ alias 'xzegrep=xzegrep --color=auto'
+++++ alias 'xzfgrep=xzfgrep --color=auto'
++++ for i in /etc/profile.d/*.sh
++++ '[' -r /etc/profile.d/colorzgrep.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/colorzgrep.sh
+++++ '[' -f /usr/libexec/grepconf.sh ']'
+++++ /usr/libexec/grepconf.sh -c
+++++ alias 'zgrep=zgrep --color=auto'
+++++ alias 'zfgrep=zfgrep --color=auto'
+++++ alias 'zegrep=zegrep --color=auto'
++++ for i in /etc/profile.d/*.sh
++++ '[' -r /etc/profile.d/debuginfod.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/debuginfod.sh
+++++ '[' -z 'https://debuginfod.centos.org/ ' ']'
++++ for i in /etc/profile.d/*.sh
++++ '[' -r /etc/profile.d/flatpak.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/flatpak.sh
+++++ command -v flatpak
++++++ unset G_MESSAGES_DEBUG
++++++ echo /home/jenkins/.local/share/flatpak
++++++ GIO_USE_VFS=local
++++++ flatpak --installations
++++++ new_dirs=
++++++ read -r install_path
++++++ share_path=/home/jenkins/.local/share/flatpak/exports/share
++++++ case ":$XDG_DATA_DIRS:" in
++++++ :
++++++ read -r install_path
++++++ share_path=/var/lib/flatpak/exports/share
++++++ case ":$XDG_DATA_DIRS:" in
++++++ :
++++++ read -r install_path
++++++ echo ''
+++++ new_dirs=
+++++ export XDG_DATA_DIRS
+++++ XDG_DATA_DIRS=/home/jenkins/.local/share/flatpak/exports/share:/var/lib/flatpak/exports/share:/usr/local/share:/usr/share
++++ for i in /etc/profile.d/*.sh
++++ '[' -r /etc/profile.d/gawk.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/gawk.sh
++++ for i in /etc/profile.d/*.sh
++++ '[' -r /etc/profile.d/gnome-ssh-askpass.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/gnome-ssh-askpass.sh
+++++ SSH_ASKPASS=/usr/libexec/openssh/gnome-ssh-askpass
+++++ export SSH_ASKPASS
++++ for i in /etc/profile.d/*.sh
++++ '[' -r /etc/profile.d/lang.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/lang.sh
+++++ '[' -n en_US.UTF-8 ']'
+++++ LANG_backup=en_US.UTF-8
+++++ for config in /etc/locale.conf "${HOME}/.i18n"
+++++ '[' -f /etc/locale.conf ']'
++++++ /usr/bin/sed -r -e 's/^[[:blank:]]*([[:upper:]_]+)=([[:print:][:digit:]\._-]+|"[[:print:][:digit:]\._-]+")/export \1=\2/;t;d' /etc/locale.conf
+++++ eval export 'LANG="en_US.UTF-8"'
++++++ export LANG=en_US.UTF-8
++++++ LANG=en_US.UTF-8
+++++ for config in /etc/locale.conf "${HOME}/.i18n"
+++++ '[' -f /home/jenkins/.i18n ']'
+++++ '[' -n en_US.UTF-8 ']'
+++++ LANG=en_US.UTF-8
+++++ unset LANG_backup config
+++++ '[' -n '' ']'
+++++ '[' -n en_US.UTF-8 ']'
+++++ '[' dumb = linux ']'
++++ for i in /etc/profile.d/*.sh
++++ '[' -r /etc/profile.d/less.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/less.sh
+++++ '[' -z '||/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/ssh-x-forwarding.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/ssh-x-forwarding.sh
+++++ '[' -z '18.18.33.14 44802 172.16.90.130 22' ']'
+++++ '[' -z 1 ']'
+++++ '[' -z '' ']'
+++++ return
++++ for i in /etc/profile.d/*.sh
++++ '[' -r /etc/profile.d/vim.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/vim.sh
+++++ '[' -n '4.4.20(1)-release' -o -n '' -o -n '' ']'
++++++ /usr/bin/id -u
+++++ '[' 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 '4.4.20(1)-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
+++++ case "$(basename $(readlink /proc/$$/exe))" in
+++++++ readlink /proc/19276/exe
++++++ basename /usr/bin/bash
+++++ which_declare='declare -f'
+++++ which_opt=-f
+++++ export which_declare
+++++ export -f which
++++ unset i
++++ unset -f pathmunge
+++ PATH=/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
+++ export PATH
++ 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/7.7/LINUX64/ESP/LINUX64
++ ESP_BLOC=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64
++ export ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64
++ ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64
++ export JULIA_DEPOT_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/julia
++ JULIA_DEPOT_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.6 != '' ]]
++ [[ '' != '' ]]
++ [[ reynolds-centOS8 == *\r\e\y\n\o\l\d\s* ]]
++ [[ '' != '' ]]
++ [[ -d /home/jenkins/util/ESP/Python/ESP_Python-3.11.6 ]]
++ [[ -d /home/jenkins/util/ESP/Python ]]
+++ ls -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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9//bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ 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-7.7.0
++ export CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.7.0
++ CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.7.0
++ export CASARCH=.
++ CASARCH=.
++ export LD_LIBRARY_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9//lib:
++ LD_LIBRARY_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.7.0/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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ PATH=/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9//bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ 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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ 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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ 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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ 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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ 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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ 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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ 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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ 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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ 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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ 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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ 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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ 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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ export CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.7/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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ 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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ [[ reynolds-centOS8 == \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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/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/7.7/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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.7/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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.7/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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.7/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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ [[ reynolds-centOS8 == \m\a\c\y\s* ]]
++ [[ reynolds-centOS8 == \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-centOS8 == \m\a\c\y\s ]]
++ [[ reynolds-centOS8 == \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/7.7/LINUX64/OpenCSM/trunk/data
++ CSMDATA=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/data
+ virtualenv /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv
created virtual environment CPython3.11.9.final.0-64 in 286ms
  creator CPython3Posix(dest=/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/ESP_venv/bin/activate
++ '[' /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/activate = /home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/ESP_venv
++ '[' linux-gnu = cygwin ']'
++ '[' linux-gnu = msys ']'
++ export VIRTUAL_ENV
++ _OLD_VIRTUAL_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.7/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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.7/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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH
++ '[' x '!=' x ']'
+++ basename /home/jenkins/workspace/ESP_Beta/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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-centOS8 == *\v\i\g\g\e\n* ]]
+ pip_install cvxopt
+ /home/jenkins/workspace/ESP_Beta/7.7/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/7.7/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/7.7/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/7.7/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_28_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_28_x86_64.whl (4.5 MB)
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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/7.7/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
--2024-04-27 17:48:42--  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: 268487989 (256M) [application/x-gzip]
Saving to: ‘ESPbeta.tgz’

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 25850K .......... .......... .......... .......... ..........  9% 18.4M 17s
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 27300K .......... .......... .......... .......... .......... 10% 90.4M 16s
 27350K .......... .......... .......... .......... .......... 10% 36.6M 16s
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 28150K .......... .......... .......... .......... .......... 10% 33.9M 16s
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 30350K .......... .......... .......... .......... .......... 11% 16.0M 16s
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 30450K .......... .......... .......... .......... .......... 11% 14.9M 16s
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 30650K .......... .......... .......... .......... .......... 11% 20.5M 16s
 30700K .......... .......... .......... .......... .......... 11% 14.5M 16s
 30750K .......... .......... .......... .......... .......... 11% 16.3M 16s
 30800K .......... .......... .......... .......... .......... 11% 19.9M 16s
 30850K .......... .......... .......... .......... .......... 11% 7.79M 16s
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 36150K .......... .......... .......... .......... .......... 13% 11.1M 17s
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 36300K .......... .......... .......... .......... .......... 13% 11.4M 17s
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 37050K .......... .......... .......... .......... .......... 14% 5.47M 17s
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 37150K .......... .......... .......... .......... .......... 14% 8.49M 17s
 37200K .......... .......... .......... .......... .......... 14% 7.31M 17s
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 37600K .......... .......... .......... .......... .......... 14% 9.48M 18s
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 37700K .......... .......... .......... .......... .......... 14% 22.4M 17s
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 37800K .......... .......... .......... .......... .......... 14% 24.2M 17s
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 38400K .......... .......... .......... .......... .......... 14% 13.1M 17s
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 38550K .......... .......... .......... .......... .......... 14% 8.58M 18s
 38600K .......... .......... .......... .......... .......... 14% 11.2M 18s
 38650K .......... .......... .......... .......... .......... 14% 9.39M 18s
 38700K .......... .......... .......... .......... .......... 14% 9.97M 18s
 38750K .......... .......... .......... .......... .......... 14% 13.2M 18s
 38800K .......... .......... .......... .......... .......... 14% 14.1M 17s
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 38900K .......... .......... .......... .......... .......... 14% 8.70M 17s
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 39100K .......... .......... .......... .......... .......... 14% 9.64M 17s
 39150K .......... .......... .......... .......... .......... 14% 13.9M 17s
 39200K .......... .......... .......... .......... .......... 14% 7.36M 17s
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 39300K .......... .......... .......... .......... .......... 15% 8.46M 17s
 39350K .......... .......... .......... .......... .......... 15% 6.61M 18s
 39400K .......... .......... .......... .......... .......... 15% 10.3M 18s
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 39500K .......... .......... .......... .......... .......... 15% 10.2M 18s
 39550K .......... .......... .......... .......... .......... 15% 6.91M 18s
 39600K .......... .......... .......... .......... .......... 15% 5.88M 18s
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 39700K .......... .......... .......... .......... .......... 15% 6.73M 18s
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 39800K .......... .......... .......... .......... .......... 15% 4.87M 18s
 39850K .......... .......... .......... .......... .......... 15% 7.22M 18s
 39900K .......... .......... .......... .......... .......... 15% 5.71M 18s
 39950K .......... .......... .......... .......... .......... 15% 5.98M 18s
 40000K .......... .......... .......... .......... .......... 15% 8.83M 18s
 40050K .......... .......... .......... .......... .......... 15% 7.90M 18s
 40100K .......... .......... .......... .......... .......... 15% 5.15M 18s
 40150K .......... .......... .......... .......... .......... 15% 8.51M 18s
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 40250K .......... .......... .......... .......... .......... 15% 6.07M 18s
 40300K .......... .......... .......... .......... .......... 15% 10.2M 18s
 40350K .......... .......... .......... .......... .......... 15% 12.2M 18s
 40400K .......... .......... .......... .......... .......... 15% 15.3M 18s
 40450K .......... .......... .......... .......... .......... 15% 10.9M 18s
 40500K .......... .......... .......... .......... .......... 15% 11.4M 18s
 40550K .......... .......... .......... .......... .......... 15% 12.5M 18s
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 40650K .......... .......... .......... .......... .......... 15% 18.1M 18s
 40700K .......... .......... .......... .......... .......... 15% 13.4M 18s
 40750K .......... .......... .......... .......... .......... 15% 14.8M 18s
 40800K .......... .......... .......... .......... .......... 15% 28.8M 18s
 40850K .......... .......... .......... .......... .......... 15% 17.6M 18s
 40900K .......... .......... .......... .......... .......... 15% 75.9M 18s
 40950K .......... .......... .......... .......... .......... 15% 37.1M 18s
 41000K .......... .......... .......... .......... .......... 15% 29.4M 18s
 41050K .......... .......... .......... .......... .......... 15% 25.8M 18s
 41100K .......... .......... .......... .......... .......... 15% 24.0M 18s
 41150K .......... .......... .......... .......... .......... 15% 16.7M 18s
 41200K .......... .......... .......... .......... .......... 15% 55.1M 18s
 41250K .......... .......... .......... .......... .......... 15% 26.2M 18s
 41300K .......... .......... .......... .......... .......... 15% 26.7M 18s
 41350K .......... .......... .......... .......... .......... 15% 21.0M 18s
 41400K .......... .......... .......... .......... .......... 15% 26.7M 18s
 41450K .......... .......... .......... .......... .......... 15% 16.8M 18s
 41500K .......... .......... .......... .......... .......... 15% 16.7M 18s
 41550K .......... .......... .......... .......... .......... 15% 18.6M 17s
 41600K .......... .......... .......... .......... .......... 15% 10.0M 18s
 41650K .......... .......... .......... .......... .......... 15% 24.6M 17s
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 41750K .......... .......... .......... .......... .......... 15% 20.8M 17s
 41800K .......... .......... .......... .......... .......... 15% 11.7M 17s
 41850K .......... .......... .......... .......... .......... 15% 9.26M 17s
 41900K .......... .......... .......... .......... .......... 15% 7.35M 17s
 41950K .......... .......... .......... .......... .......... 16% 11.2M 17s
 42000K .......... .......... .......... .......... .......... 16% 6.48M 17s
 42050K .......... .......... .......... .......... .......... 16% 8.29M 17s
 42100K .......... .......... .......... .......... .......... 16% 7.94M 18s
 42150K .......... .......... .......... .......... .......... 16% 9.52M 18s
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 42250K .......... .......... .......... .......... .......... 16% 9.45M 18s
 42300K .......... .......... .......... .......... .......... 16% 7.52M 18s
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 42500K .......... .......... .......... .......... .......... 16% 5.73M 18s
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 42600K .......... .......... .......... .......... .......... 16% 6.27M 18s
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 42700K .......... .......... .......... .......... .......... 16% 4.43M 18s
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 42900K .......... .......... .......... .......... .......... 16% 8.21M 18s
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 43150K .......... .......... .......... .......... .......... 16% 5.32M 18s
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 43650K .......... .......... .......... .......... .......... 16% 8.22M 18s
 43700K .......... .......... .......... .......... .......... 16% 6.91M 18s
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 43800K .......... .......... .......... .......... .......... 16% 6.31M 18s
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 44150K .......... .......... .......... .......... .......... 16% 7.26M 18s
 44200K .......... .......... .......... .......... .......... 16% 6.38M 18s
 44250K .......... .......... .......... .......... .......... 16% 9.61M 18s
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 44700K .......... .......... .......... .......... .......... 17% 3.73M 18s
 44750K .......... .......... .......... .......... .......... 17% 5.17M 18s
 44800K .......... .......... .......... .......... .......... 17% 4.89M 18s
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 44900K .......... .......... .......... .......... .......... 17% 6.48M 18s
 44950K .......... .......... .......... .......... .......... 17% 3.97M 18s
 45000K .......... .......... .......... .......... .......... 17% 10.5M 18s
 45050K .......... .......... .......... .......... .......... 17% 5.61M 18s
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 45150K .......... .......... .......... .......... .......... 17% 6.34M 18s
 45200K .......... .......... .......... .......... .......... 17% 5.82M 19s
 45250K .......... .......... .......... .......... .......... 17% 9.85M 19s
 45300K .......... .......... .......... .......... .......... 17% 6.91M 19s
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 45400K .......... .......... .......... .......... .......... 17% 8.72M 19s
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 45500K .......... .......... .......... .......... .......... 17% 9.83M 19s
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 45600K .......... .......... .......... .......... .......... 17% 6.83M 19s
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 45700K .......... .......... .......... .......... .......... 17% 7.10M 19s
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 45800K .......... .......... .......... .......... .......... 17% 8.23M 19s
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 45900K .......... .......... .......... .......... .......... 17% 11.8M 19s
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 46250K .......... .......... .......... .......... .......... 17% 12.0M 19s
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 46800K .......... .......... .......... .......... .......... 17% 11.9M 19s
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 46900K .......... .......... .......... .......... .......... 17% 10.3M 19s
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 47000K .......... .......... .......... .......... .......... 17% 5.94M 19s
 47050K .......... .......... .......... .......... .......... 17% 10.7M 19s
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 47150K .......... .......... .......... .......... .......... 18% 10.1M 19s
 47200K .......... .......... .......... .......... .......... 18% 6.21M 19s
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 47300K .......... .......... .......... .......... .......... 18% 10.4M 19s
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 47900K .......... .......... .......... .......... .......... 18% 11.6M 19s
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 48100K .......... .......... .......... .......... .......... 18% 7.11M 19s
 48150K .......... .......... .......... .......... .......... 18% 5.35M 19s
 48200K .......... .......... .......... .......... .......... 18% 12.2M 19s
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 48300K .......... .......... .......... .......... .......... 18% 7.13M 19s
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 49300K .......... .......... .......... .......... .......... 18% 76.3M 19s
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 50150K .......... .......... .......... .......... .......... 19% 11.6M 19s
 50200K .......... .......... .......... .......... .......... 19% 5.42M 19s
 50250K .......... .......... .......... .......... .......... 19% 10.7M 19s
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 50350K .......... .......... .......... .......... .......... 19% 7.41M 19s
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 50650K .......... .......... .......... .......... .......... 19% 8.87M 19s
 50700K .......... .......... .......... .......... .......... 19% 10.2M 19s
 50750K .......... .......... .......... .......... .......... 19% 5.74M 19s
 50800K .......... .......... .......... .......... .......... 19% 13.3M 19s
 50850K .......... .......... .......... .......... .......... 19% 6.58M 19s
 50900K .......... .......... .......... .......... .......... 19% 8.35M 19s
 50950K .......... .......... .......... .......... .......... 19% 5.68M 19s
 51000K .......... .......... .......... .......... .......... 19% 7.07M 19s
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 51100K .......... .......... .......... .......... .......... 19% 7.41M 19s
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 51200K .......... .......... .......... .......... .......... 19% 9.16M 19s
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 51400K .......... .......... .......... .......... .......... 19% 10.2M 19s
 51450K .......... .......... .......... .......... .......... 19% 7.19M 19s
 51500K .......... .......... .......... .......... .......... 19% 5.77M 19s
 51550K .......... .......... .......... .......... .......... 19% 7.19M 19s
 51600K .......... .......... .......... .......... .......... 19% 5.73M 19s
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 51750K .......... .......... .......... .......... .......... 19% 8.39M 19s
 51800K .......... .......... .......... .......... .......... 19% 7.04M 19s
 51850K .......... .......... .......... .......... .......... 19% 7.78M 19s
 51900K .......... .......... .......... .......... .......... 19% 8.45M 19s
 51950K .......... .......... .......... .......... .......... 19% 6.07M 19s
 52000K .......... .......... .......... .......... .......... 19% 10.3M 19s
 52050K .......... .......... .......... .......... .......... 19% 7.92M 19s
 52100K .......... .......... .......... .......... .......... 19% 7.63M 19s
 52150K .......... .......... .......... .......... .......... 19% 10.7M 19s
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 52300K .......... .......... .......... .......... .......... 19% 11.9M 19s
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 52400K .......... .......... .......... .......... .......... 20% 11.0M 19s
 52450K .......... .......... .......... .......... .......... 20% 8.63M 19s
 52500K .......... .......... .......... .......... .......... 20% 10.4M 19s
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 52650K .......... .......... .......... .......... .......... 20% 12.2M 19s
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 52950K .......... .......... .......... .......... .......... 20% 13.9M 19s
 53000K .......... .......... .......... .......... .......... 20% 12.8M 19s
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 53100K .......... .......... .......... .......... .......... 20% 11.5M 19s
 53150K .......... .......... .......... .......... .......... 20% 14.1M 19s
 53200K .......... .......... .......... .......... .......... 20% 29.5M 19s
 53250K .......... .......... .......... .......... .......... 20% 10.0M 19s
 53300K .......... .......... .......... .......... .......... 20% 12.7M 19s
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 53500K .......... .......... .......... .......... .......... 20% 14.5M 19s
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 53600K .......... .......... .......... .......... .......... 20% 11.3M 19s
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 53700K .......... .......... .......... .......... .......... 20% 4.93M 19s
 53750K .......... .......... .......... .......... .......... 20%  110M 19s
 53800K .......... .......... .......... .......... .......... 20% 14.1M 19s
 53850K .......... .......... .......... .......... .......... 20% 9.77M 19s
 53900K .......... .......... .......... .......... .......... 20% 10.9M 19s
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 54050K .......... .......... .......... .......... .......... 20% 11.3M 19s
 54100K .......... .......... .......... .......... .......... 20% 7.94M 19s
 54150K .......... .......... .......... .......... .......... 20% 12.2M 19s
 54200K .......... .......... .......... .......... .......... 20% 8.77M 19s
 54250K .......... .......... .......... .......... .......... 20% 12.3M 19s
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 54500K .......... .......... .......... .......... .......... 20% 5.80M 19s
 54550K .......... .......... .......... .......... .......... 20% 82.2M 19s
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 97450K .......... .......... .......... .......... .......... 37% 11.2M 19s
 97500K .......... .......... .......... .......... .......... 37% 26.9M 19s
 97550K .......... .......... .......... .......... .......... 37% 20.0M 19s
 97600K .......... .......... .......... .......... .......... 37% 11.9M 19s
 97650K .......... .......... .......... .......... .......... 37% 12.0M 19s
 97700K .......... .......... .......... .......... .......... 37% 8.54M 19s
 97750K .......... .......... .......... .......... .......... 37% 13.2M 19s
 97800K .......... .......... .......... .......... .......... 37% 25.0M 19s
 97850K .......... .......... .......... .......... .......... 37% 9.69M 19s
 97900K .......... .......... .......... .......... .......... 37% 14.1M 19s
 97950K .......... .......... .......... .......... .......... 37% 18.0M 19s
 98000K .......... .......... .......... .......... .......... 37% 11.8M 19s
 98050K .......... .......... .......... .......... .......... 37% 9.71M 19s
 98100K .......... .......... .......... .......... .......... 37% 2.01M 19s
 98150K .......... .......... .......... .......... .......... 37% 7.09M 19s
 98200K .......... .......... .......... .......... .......... 37% 5.51M 19s
 98250K .......... .......... .......... .......... .......... 37% 4.58M 19s
 98300K .......... .......... .......... .......... .......... 37% 4.03M 19s
 98350K .......... .......... .......... .......... .......... 37% 3.68M 19s
 98400K .......... .......... .......... .......... .......... 37% 6.15M 19s
 98450K .......... .......... .......... .......... .......... 37% 9.61M 19s
 98500K .......... .......... .......... .......... .......... 37% 9.18M 19s
 98550K .......... .......... .......... .......... .......... 37% 13.0M 19s
 98600K .......... .......... .......... .......... .......... 37% 10.5M 19s
 98650K .......... .......... .......... .......... .......... 37% 14.8M 19s
 98700K .......... .......... .......... .......... .......... 37% 13.0M 19s
 98750K .......... .......... .......... .......... .......... 37% 12.5M 19s
 98800K .......... .......... .......... .......... .......... 37% 11.5M 19s
 98850K .......... .......... .......... .......... .......... 37% 14.5M 19s
 98900K .......... .......... .......... .......... .......... 37% 15.8M 19s
 98950K .......... .......... .......... .......... .......... 37% 10.6M 19s
 99000K .......... .......... .......... .......... .......... 37% 12.4M 19s
 99050K .......... .......... .......... .......... .......... 37% 11.7M 19s
 99100K .......... .......... .......... .......... .......... 37% 11.8M 19s
 99150K .......... .......... .......... .......... .......... 37% 14.1M 19s
 99200K .......... .......... .......... .......... .......... 37% 11.0M 19s
 99250K .......... .......... .......... .......... .......... 37% 17.6M 19s
 99300K .......... .......... .......... .......... .......... 37% 19.7M 19s
 99350K .......... .......... .......... .......... .......... 37% 10.3M 19s
 99400K .......... .......... .......... .......... .......... 37% 19.3M 19s
 99450K .......... .......... .......... .......... .......... 37% 13.7M 19s
 99500K .......... .......... .......... .......... .......... 37% 15.6M 19s
 99550K .......... .......... .......... .......... .......... 37% 20.4M 19s
 99600K .......... .......... .......... .......... .......... 38% 10.0M 19s
 99650K .......... .......... .......... .......... .......... 38% 17.7M 19s
 99700K .......... .......... .......... .......... .......... 38% 10.5M 19s
 99750K .......... .......... .......... .......... .......... 38% 8.85M 19s
 99800K .......... .......... .......... .......... .......... 38% 10.4M 19s
 99850K .......... .......... .......... .......... .......... 38% 9.76M 19s
 99900K .......... .......... .......... .......... .......... 38% 12.8M 19s
 99950K .......... .......... .......... .......... .......... 38% 10.4M 19s
100000K .......... .......... .......... .......... .......... 38% 9.17M 19s
100050K .......... .......... .......... .......... .......... 38% 12.4M 19s
100100K .......... .......... .......... .......... .......... 38% 13.7M 19s
100150K .......... .......... .......... .......... .......... 38% 9.41M 19s
100200K .......... .......... .......... .......... .......... 38% 11.8M 19s
100250K .......... .......... .......... .......... .......... 38% 11.2M 19s
100300K .......... .......... .......... .......... .......... 38% 20.8M 19s
100350K .......... .......... .......... .......... .......... 38% 21.9M 19s
100400K .......... .......... .......... .......... .......... 38% 23.8M 19s
100450K .......... .......... .......... .......... .......... 38% 17.1M 19s
100500K .......... .......... .......... .......... .......... 38% 14.4M 19s
100550K .......... .......... .......... .......... .......... 38% 18.2M 19s
100600K .......... .......... .......... .......... .......... 38% 7.80M 19s
100650K .......... .......... .......... .......... .......... 38% 11.1M 19s
100700K .......... .......... .......... .......... .......... 38% 12.0M 19s
100750K .......... .......... .......... .......... .......... 38% 19.0M 19s
100800K .......... .......... .......... .......... .......... 38% 20.6M 19s
100850K .......... .......... .......... .......... .......... 38% 16.7M 19s
100900K .......... .......... .......... .......... .......... 38% 15.4M 19s
100950K .......... .......... .......... .......... .......... 38% 12.6M 19s
101000K .......... .......... .......... .......... .......... 38% 13.2M 19s
101050K .......... .......... .......... .......... .......... 38% 13.9M 19s
101100K .......... .......... .......... .......... .......... 38% 7.62M 19s
101150K .......... .......... .......... .......... .......... 38% 14.4M 19s
101200K .......... .......... .......... .......... .......... 38% 10.3M 19s
101250K .......... .......... .......... .......... .......... 38% 12.5M 19s
101300K .......... .......... .......... .......... .......... 38% 18.5M 19s
101350K .......... .......... .......... .......... .......... 38% 17.2M 19s
101400K .......... .......... .......... .......... .......... 38% 14.0M 19s
101450K .......... .......... .......... .......... .......... 38% 11.6M 19s
101500K .......... .......... .......... .......... .......... 38% 14.1M 19s
101550K .......... .......... .......... .......... .......... 38% 14.9M 19s
101600K .......... .......... .......... .......... .......... 38% 11.6M 19s
101650K .......... .......... .......... .......... .......... 38% 19.4M 18s
101700K .......... .......... .......... .......... .......... 38% 18.0M 18s
101750K .......... .......... .......... .......... .......... 38% 20.5M 18s
101800K .......... .......... .......... .......... .......... 38% 17.8M 18s
101850K .......... .......... .......... .......... .......... 38% 15.4M 18s
101900K .......... .......... .......... .......... .......... 38% 20.6M 18s
101950K .......... .......... .......... .......... .......... 38% 20.2M 18s
102000K .......... .......... .......... .......... .......... 38% 13.6M 18s
102050K .......... .......... .......... .......... .......... 38% 32.5M 18s
102100K .......... .......... .......... .......... .......... 38% 16.2M 18s
102150K .......... .......... .......... .......... .......... 38% 15.2M 18s
102200K .......... .......... .......... .......... .......... 38% 8.94M 18s
102250K .......... .......... .......... .......... .......... 39% 15.7M 18s
102300K .......... .......... .......... .......... .......... 39% 17.2M 18s
102350K .......... .......... .......... .......... .......... 39% 19.4M 18s
102400K .......... .......... .......... .......... .......... 39% 18.1M 18s
102450K .......... .......... .......... .......... .......... 39% 18.8M 18s
102500K .......... .......... .......... .......... .......... 39% 15.4M 18s
102550K .......... .......... .......... .......... .......... 39% 18.2M 18s
102600K .......... .......... .......... .......... .......... 39% 19.5M 18s
102650K .......... .......... .......... .......... .......... 39% 19.4M 18s
102700K .......... .......... .......... .......... .......... 39% 14.3M 18s
102750K .......... .......... .......... .......... .......... 39% 19.4M 18s
102800K .......... .......... .......... .......... .......... 39% 22.8M 18s
102850K .......... .......... .......... .......... .......... 39% 16.7M 18s
102900K .......... .......... .......... .......... .......... 39% 20.2M 18s
102950K .......... .......... .......... .......... .......... 39% 17.5M 18s
103000K .......... .......... .......... .......... .......... 39% 22.2M 18s
103050K .......... .......... .......... .......... .......... 39% 19.1M 18s
103100K .......... .......... .......... .......... .......... 39% 17.6M 18s
103150K .......... .......... .......... .......... .......... 39% 17.9M 18s
103200K .......... .......... .......... .......... .......... 39% 11.6M 18s
103250K .......... .......... .......... .......... .......... 39% 22.7M 18s
103300K .......... .......... .......... .......... .......... 39% 35.7M 18s
103350K .......... .......... .......... .......... .......... 39% 19.5M 18s
103400K .......... .......... .......... .......... .......... 39% 14.8M 18s
103450K .......... .......... .......... .......... .......... 39% 34.2M 18s
103500K .......... .......... .......... .......... .......... 39% 21.2M 18s
103550K .......... .......... .......... .......... .......... 39% 13.2M 18s
103600K .......... .......... .......... .......... .......... 39% 17.7M 18s
103650K .......... .......... .......... .......... .......... 39% 15.4M 18s
103700K .......... .......... .......... .......... .......... 39% 10.0M 18s
103750K .......... .......... .......... .......... .......... 39% 13.8M 18s
103800K .......... .......... .......... .......... .......... 39% 20.9M 18s
103850K .......... .......... .......... .......... .......... 39% 13.0M 18s
103900K .......... .......... .......... .......... .......... 39% 17.2M 18s
103950K .......... .......... .......... .......... .......... 39% 13.4M 18s
104000K .......... .......... .......... .......... .......... 39% 19.9M 18s
104050K .......... .......... .......... .......... .......... 39% 16.4M 18s
104100K .......... .......... .......... .......... .......... 39% 12.8M 18s
104150K .......... .......... .......... .......... .......... 39% 11.7M 18s
104200K .......... .......... .......... .......... .......... 39% 12.8M 18s
104250K .......... .......... .......... .......... .......... 39% 7.96M 18s
104300K .......... .......... .......... .......... .......... 39% 15.5M 18s
104350K .......... .......... .......... .......... .......... 39% 11.7M 18s
104400K .......... .......... .......... .......... .......... 39% 17.0M 18s
104450K .......... .......... .......... .......... .......... 39% 10.5M 18s
104500K .......... .......... .......... .......... .......... 39% 15.0M 18s
104550K .......... .......... .......... .......... .......... 39% 10.8M 18s
104600K .......... .......... .......... .......... .......... 39% 13.6M 18s
104650K .......... .......... .......... .......... .......... 39% 17.2M 18s
104700K .......... .......... .......... .......... .......... 39% 14.4M 18s
104750K .......... .......... .......... .......... .......... 39% 14.6M 18s
104800K .......... .......... .......... .......... .......... 39% 12.4M 18s
104850K .......... .......... .......... .......... .......... 40% 9.97M 18s
104900K .......... .......... .......... .......... .......... 40% 17.8M 18s
104950K .......... .......... .......... .......... .......... 40% 18.1M 18s
105000K .......... .......... .......... .......... .......... 40% 23.5M 18s
105050K .......... .......... .......... .......... .......... 40% 14.4M 18s
105100K .......... .......... .......... .......... .......... 40% 6.95M 18s
105150K .......... .......... .......... .......... .......... 40% 9.76M 18s
105200K .......... .......... .......... .......... .......... 40% 13.5M 18s
105250K .......... .......... .......... .......... .......... 40% 12.1M 18s
105300K .......... .......... .......... .......... .......... 40% 10.7M 18s
105350K .......... .......... .......... .......... .......... 40% 7.00M 18s
105400K .......... .......... .......... .......... .......... 40% 10.7M 18s
105450K .......... .......... .......... .......... .......... 40% 6.57M 18s
105500K .......... .......... .......... .......... .......... 40% 18.8M 18s
105550K .......... .......... .......... .......... .......... 40% 10.8M 18s
105600K .......... .......... .......... .......... .......... 40% 9.81M 18s
105650K .......... .......... .......... .......... .......... 40%  950K 18s
105700K .......... .......... .......... .......... .......... 40% 5.75M 18s
105750K .......... .......... .......... .......... .......... 40% 13.3M 18s
105800K .......... .......... .......... .......... .......... 40% 10.1M 18s
105850K .......... .......... .......... .......... .......... 40% 8.80M 18s
105900K .......... .......... .......... .......... .......... 40% 18.0M 18s
105950K .......... .......... .......... .......... .......... 40% 13.8M 18s
106000K .......... .......... .......... .......... .......... 40% 10.8M 18s
106050K .......... .......... .......... .......... .......... 40% 10.6M 18s
106100K .......... .......... .......... .......... .......... 40% 7.53M 18s
106150K .......... .......... .......... .......... .......... 40% 10.9M 18s
106200K .......... .......... .......... .......... .......... 40% 6.53M 18s
106250K .......... .......... .......... .......... .......... 40% 6.63M 18s
106300K .......... .......... .......... .......... .......... 40% 6.99M 18s
106350K .......... .......... .......... .......... .......... 40% 14.5M 18s
106400K .......... .......... .......... .......... .......... 40% 16.1M 18s
106450K .......... .......... .......... .......... .......... 40% 11.7M 18s
106500K .......... .......... .......... .......... .......... 40% 17.1M 18s
106550K .......... .......... .......... .......... .......... 40% 25.7M 18s
106600K .......... .......... .......... .......... .......... 40% 11.4M 18s
106650K .......... .......... .......... .......... .......... 40% 33.7M 18s
106700K .......... .......... .......... .......... .......... 40% 13.8M 18s
106750K .......... .......... .......... .......... .......... 40% 9.66M 18s
106800K .......... .......... .......... .......... .......... 40% 7.89M 18s
106850K .......... .......... .......... .......... .......... 40% 15.6M 18s
106900K .......... .......... .......... .......... .......... 40% 18.9M 18s
106950K .......... .......... .......... .......... .......... 40% 14.1M 18s
107000K .......... .......... .......... .......... .......... 40% 17.0M 18s
107050K .......... .......... .......... .......... .......... 40% 16.9M 18s
107100K .......... .......... .......... .......... .......... 40% 10.2M 18s
107150K .......... .......... .......... .......... .......... 40% 16.8M 18s
107200K .......... .......... .......... .......... .......... 40% 10.6M 18s
107250K .......... .......... .......... .......... .......... 40% 9.35M 18s
107300K .......... .......... .......... .......... .......... 40% 12.7M 18s
107350K .......... .......... .......... .......... .......... 40% 9.42M 18s
107400K .......... .......... .......... .......... .......... 40% 12.0M 18s
107450K .......... .......... .......... .......... .......... 40% 16.1M 18s
107500K .......... .......... .......... .......... .......... 41% 21.3M 18s
107550K .......... .......... .......... .......... .......... 41% 16.3M 18s
107600K .......... .......... .......... .......... .......... 41% 15.7M 18s
107650K .......... .......... .......... .......... .......... 41% 16.0M 18s
107700K .......... .......... .......... .......... .......... 41% 19.0M 17s
107750K .......... .......... .......... .......... .......... 41% 19.5M 17s
107800K .......... .......... .......... .......... .......... 41% 30.3M 17s
107850K .......... .......... .......... .......... .......... 41% 13.6M 17s
107900K .......... .......... .......... .......... .......... 41% 13.9M 17s
107950K .......... .......... .......... .......... .......... 41% 11.0M 17s
108000K .......... .......... .......... .......... .......... 41% 10.5M 17s
108050K .......... .......... .......... .......... .......... 41% 15.7M 17s
108100K .......... .......... .......... .......... .......... 41% 13.5M 17s
108150K .......... .......... .......... .......... .......... 41% 25.4M 17s
108200K .......... .......... .......... .......... .......... 41% 19.0M 17s
108250K .......... .......... .......... .......... .......... 41% 24.7M 17s
108300K .......... .......... .......... .......... .......... 41% 24.0M 17s
108350K .......... .......... .......... .......... .......... 41% 22.2M 17s
108400K .......... .......... .......... .......... .......... 41% 22.5M 17s
108450K .......... .......... .......... .......... .......... 41% 21.1M 17s
108500K .......... .......... .......... .......... .......... 41% 16.4M 17s
108550K .......... .......... .......... .......... .......... 41% 18.6M 17s
108600K .......... .......... .......... .......... .......... 41% 13.8M 17s
108650K .......... .......... .......... .......... .......... 41% 17.3M 17s
108700K .......... .......... .......... .......... .......... 41% 15.9M 17s
108750K .......... .......... .......... .......... .......... 41% 21.1M 17s
108800K .......... .......... .......... .......... .......... 41% 19.5M 17s
108850K .......... .......... .......... .......... .......... 41% 19.2M 17s
108900K .......... .......... .......... .......... .......... 41% 11.1M 17s
108950K .......... .......... .......... .......... .......... 41% 9.05M 17s
109000K .......... .......... .......... .......... .......... 41% 18.6M 17s
109050K .......... .......... .......... .......... .......... 41% 11.1M 17s
109100K .......... .......... .......... .......... .......... 41% 14.0M 17s
109150K .......... .......... .......... .......... .......... 41% 22.0M 17s
109200K .......... .......... .......... .......... .......... 41% 16.5M 17s
109250K .......... .......... .......... .......... .......... 41% 20.5M 17s
109300K .......... .......... .......... .......... .......... 41% 20.0M 17s
109350K .......... .......... .......... .......... .......... 41% 13.0M 17s
109400K .......... .......... .......... .......... .......... 41% 17.5M 17s
109450K .......... .......... .......... .......... .......... 41% 19.6M 17s
109500K .......... .......... .......... .......... .......... 41% 23.4M 17s
109550K .......... .......... .......... .......... .......... 41% 23.0M 17s
109600K .......... .......... .......... .......... .......... 41% 23.1M 17s
109650K .......... .......... .......... .......... .......... 41% 20.9M 17s
109700K .......... .......... .......... .......... .......... 41% 13.6M 17s
109750K .......... .......... .......... .......... .......... 41% 12.3M 17s
109800K .......... .......... .......... .......... .......... 41% 8.35M 17s
109850K .......... .......... .......... .......... .......... 41% 11.0M 17s
109900K .......... .......... .......... .......... .......... 41% 8.83M 17s
109950K .......... .......... .......... .......... .......... 41% 12.0M 17s
110000K .......... .......... .......... .......... .......... 41% 10.2M 17s
110050K .......... .......... .......... .......... .......... 41% 10.2M 17s
110100K .......... .......... .......... .......... .......... 42% 9.92M 17s
110150K .......... .......... .......... .......... .......... 42% 12.2M 17s
110200K .......... .......... .......... .......... .......... 42% 7.16M 17s
110250K .......... .......... .......... .......... .......... 42% 10.3M 17s
110300K .......... .......... .......... .......... .......... 42% 10.8M 17s
110350K .......... .......... .......... .......... .......... 42% 12.5M 17s
110400K .......... .......... .......... .......... .......... 42% 16.7M 17s
110450K .......... .......... .......... .......... .......... 42% 11.7M 17s
110500K .......... .......... .......... .......... .......... 42% 20.6M 17s
110550K .......... .......... .......... .......... .......... 42% 19.9M 17s
110600K .......... .......... .......... .......... .......... 42% 16.8M 17s
110650K .......... .......... .......... .......... .......... 42% 23.4M 17s
110700K .......... .......... .......... .......... .......... 42% 27.7M 17s
110750K .......... .......... .......... .......... .......... 42% 19.6M 17s
110800K .......... .......... .......... .......... .......... 42% 15.2M 17s
110850K .......... .......... .......... .......... .......... 42% 17.2M 17s
110900K .......... .......... .......... .......... .......... 42% 14.8M 17s
110950K .......... .......... .......... .......... .......... 42% 11.5M 17s
111000K .......... .......... .......... .......... .......... 42% 18.7M 17s
111050K .......... .......... .......... .......... .......... 42% 18.9M 17s
111100K .......... .......... .......... .......... .......... 42% 13.8M 17s
111150K .......... .......... .......... .......... .......... 42% 13.0M 17s
111200K .......... .......... .......... .......... .......... 42% 13.5M 17s
111250K .......... .......... .......... .......... .......... 42% 13.7M 17s
111300K .......... .......... .......... .......... .......... 42% 10.9M 17s
111350K .......... .......... .......... .......... .......... 42% 7.19M 17s
111400K .......... .......... .......... .......... .......... 42% 12.5M 17s
111450K .......... .......... .......... .......... .......... 42% 10.4M 17s
111500K .......... .......... .......... .......... .......... 42% 9.48M 17s
111550K .......... .......... .......... .......... .......... 42% 8.63M 17s
111600K .......... .......... .......... .......... .......... 42% 7.03M 17s
111650K .......... .......... .......... .......... .......... 42% 6.58M 17s
111700K .......... .......... .......... .......... .......... 42% 10.4M 17s
111750K .......... .......... .......... .......... .......... 42% 7.35M 17s
111800K .......... .......... .......... .......... .......... 42% 13.6M 17s
111850K .......... .......... .......... .......... .......... 42% 12.0M 17s
111900K .......... .......... .......... .......... .......... 42% 14.9M 17s
111950K .......... .......... .......... .......... .......... 42% 15.3M 17s
112000K .......... .......... .......... .......... .......... 42% 19.1M 17s
112050K .......... .......... .......... .......... .......... 42% 17.0M 17s
112100K .......... .......... .......... .......... .......... 42% 12.5M 17s
112150K .......... .......... .......... .......... .......... 42% 28.7M 17s
112200K .......... .......... .......... .......... .......... 42% 14.6M 17s
112250K .......... .......... .......... .......... .......... 42% 16.7M 17s
112300K .......... .......... .......... .......... .......... 42% 15.2M 17s
112350K .......... .......... .......... .......... .......... 42% 17.3M 17s
112400K .......... .......... .......... .......... .......... 42% 15.7M 17s
112450K .......... .......... .......... .......... .......... 42% 18.5M 17s
112500K .......... .......... .......... .......... .......... 42% 18.4M 17s
112550K .......... .......... .......... .......... .......... 42% 14.5M 17s
112600K .......... .......... .......... .......... .......... 42% 13.7M 17s
112650K .......... .......... .......... .......... .......... 42% 18.4M 17s
112700K .......... .......... .......... .......... .......... 43% 16.0M 17s
112750K .......... .......... .......... .......... .......... 43% 16.5M 17s
112800K .......... .......... .......... .......... .......... 43% 12.2M 17s
112850K .......... .......... .......... .......... .......... 43% 10.8M 17s
112900K .......... .......... .......... .......... .......... 43% 9.88M 17s
112950K .......... .......... .......... .......... .......... 43% 8.83M 17s
113000K .......... .......... .......... .......... .......... 43% 11.5M 17s
113050K .......... .......... .......... .......... .......... 43% 10.4M 17s
113100K .......... .......... .......... .......... .......... 43% 10.6M 17s
113150K .......... .......... .......... .......... .......... 43% 15.8M 17s
113200K .......... .......... .......... .......... .......... 43% 11.4M 17s
113250K .......... .......... .......... .......... .......... 43% 10.5M 17s
113300K .......... .......... .......... .......... .......... 43% 12.8M 17s
113350K .......... .......... .......... .......... .......... 43% 11.9M 17s
113400K .......... .......... .......... .......... .......... 43% 7.67M 17s
113450K .......... .......... .......... .......... .......... 43% 9.80M 17s
113500K .......... .......... .......... .......... .......... 43%  436K 17s
113550K .......... .......... .......... .......... .......... 43%  705K 17s
113600K .......... .......... .......... .......... .......... 43% 7.15M 17s
113650K .......... .......... .......... .......... .......... 43% 14.7M 17s
113700K .......... .......... .......... .......... .......... 43% 21.6M 17s
113750K .......... .......... .......... .......... .......... 43% 25.6M 17s
113800K .......... .......... .......... .......... .......... 43% 23.5M 17s
113850K .......... .......... .......... .......... .......... 43% 30.9M 17s
113900K .......... .......... .......... .......... .......... 43% 10.1M 17s
113950K .......... .......... .......... .......... .......... 43% 14.0M 17s
114000K .......... .......... .......... .......... .......... 43% 13.7M 17s
114050K .......... .......... .......... .......... .......... 43% 13.0M 17s
114100K .......... .......... .......... .......... .......... 43% 20.2M 17s
114150K .......... .......... .......... .......... .......... 43% 12.9M 17s
114200K .......... .......... .......... .......... .......... 43% 18.5M 17s
114250K .......... .......... .......... .......... .......... 43% 16.2M 17s
114300K .......... .......... .......... .......... .......... 43% 2.57M 17s
114350K .......... .......... .......... .......... .......... 43% 8.15M 17s
114400K .......... .......... .......... .......... .......... 43% 12.6M 17s
114450K .......... .......... .......... .......... .......... 43% 20.1M 17s
114500K .......... .......... .......... .......... .......... 43% 18.0M 17s
114550K .......... .......... .......... .......... .......... 43% 11.8M 17s
114600K .......... .......... .......... .......... .......... 43% 12.9M 17s
114650K .......... .......... .......... .......... .......... 43% 15.5M 17s
114700K .......... .......... .......... .......... .......... 43% 15.5M 17s
114750K .......... .......... .......... .......... .......... 43% 17.5M 17s
114800K .......... .......... .......... .......... .......... 43% 17.5M 17s
114850K .......... .......... .......... .......... .......... 43% 9.34M 17s
114900K .......... .......... .......... .......... .......... 43% 11.5M 17s
114950K .......... .......... .......... .......... .......... 43% 14.8M 17s
115000K .......... .......... .......... .......... .......... 43% 19.8M 17s
115050K .......... .......... .......... .......... .......... 43% 16.7M 17s
115100K .......... .......... .......... .......... .......... 43% 8.01M 17s
115150K .......... .......... .......... .......... .......... 43% 13.6M 17s
115200K .......... .......... .......... .......... .......... 43% 13.2M 16s
115250K .......... .......... .......... .......... .......... 43% 16.8M 16s
115300K .......... .......... .......... .......... .......... 43% 13.2M 16s
115350K .......... .......... .......... .......... .......... 44% 15.2M 16s
115400K .......... .......... .......... .......... .......... 44% 20.4M 16s
115450K .......... .......... .......... .......... .......... 44% 19.1M 16s
115500K .......... .......... .......... .......... .......... 44% 16.7M 16s
115550K .......... .......... .......... .......... .......... 44% 18.8M 16s
115600K .......... .......... .......... .......... .......... 44% 15.0M 16s
115650K .......... .......... .......... .......... .......... 44% 24.1M 16s
115700K .......... .......... .......... .......... .......... 44% 12.3M 16s
115750K .......... .......... .......... .......... .......... 44% 20.8M 16s
115800K .......... .......... .......... .......... .......... 44% 14.3M 16s
115850K .......... .......... .......... .......... .......... 44% 13.2M 16s
115900K .......... .......... .......... .......... .......... 44% 14.2M 16s
115950K .......... .......... .......... .......... .......... 44% 10.3M 16s
116000K .......... .......... .......... .......... .......... 44% 11.1M 16s
116050K .......... .......... .......... .......... .......... 44% 10.3M 16s
116100K .......... .......... .......... .......... .......... 44% 1.52M 16s
116150K .......... .......... .......... .......... .......... 44% 5.12M 16s
116200K .......... .......... .......... .......... .......... 44% 1.13M 16s
116250K .......... .......... .......... .......... .......... 44% 1.92M 16s
116300K .......... .......... .......... .......... .......... 44% 1.77M 16s
116350K .......... .......... .......... .......... .......... 44% 3.09M 16s
116400K .......... .......... .......... .......... .......... 44% 1.93M 16s
116450K .......... .......... .......... .......... .......... 44%  219K 17s
116500K .......... .......... .......... .......... .......... 44% 10.5M 17s
116550K .......... .......... .......... .......... .......... 44% 12.1M 17s
116600K .......... .......... .......... .......... .......... 44% 11.4M 17s
116650K .......... .......... .......... .......... .......... 44% 16.2M 17s
116700K .......... .......... .......... .......... .......... 44% 15.8M 17s
116750K .......... .......... .......... .......... .......... 44% 15.7M 17s
116800K .......... .......... .......... .......... .......... 44% 12.9M 17s
116850K .......... .......... .......... .......... .......... 44% 13.4M 17s
116900K .......... .......... .......... .......... .......... 44% 18.1M 17s
116950K .......... .......... .......... .......... .......... 44% 12.3M 17s
117000K .......... .......... .......... .......... .......... 44% 21.1M 17s
117050K .......... .......... .......... .......... .......... 44% 20.4M 17s
117100K .......... .......... .......... .......... .......... 44% 15.0M 17s
117150K .......... .......... .......... .......... .......... 44% 13.9M 17s
117200K .......... .......... .......... .......... .......... 44% 15.4M 17s
117250K .......... .......... .......... .......... .......... 44% 15.2M 17s
117300K .......... .......... .......... .......... .......... 44% 13.5M 17s
117350K .......... .......... .......... .......... .......... 44% 18.8M 17s
117400K .......... .......... .......... .......... .......... 44% 30.5M 17s
117450K .......... .......... .......... .......... .......... 44% 20.6M 17s
117500K .......... .......... .......... .......... .......... 44% 19.4M 17s
117550K .......... .......... .......... .......... .......... 44% 27.1M 17s
117600K .......... .......... .......... .......... .......... 44% 12.7M 17s
117650K .......... .......... .......... .......... .......... 44% 11.5M 17s
117700K .......... .......... .......... .......... .......... 44% 11.3M 17s
117750K .......... .......... .......... .......... .......... 44% 14.6M 17s
117800K .......... .......... .......... .......... .......... 44% 14.4M 17s
117850K .......... .......... .......... .......... .......... 44% 11.6M 17s
117900K .......... .......... .......... .......... .......... 44% 12.8M 17s
117950K .......... .......... .......... .......... .......... 45% 9.82M 16s
118000K .......... .......... .......... .......... .......... 45% 13.5M 16s
118050K .......... .......... .......... .......... .......... 45% 20.4M 16s
118100K .......... .......... .......... .......... .......... 45% 16.6M 16s
118150K .......... .......... .......... .......... .......... 45% 20.4M 16s
118200K .......... .......... .......... .......... .......... 45% 14.4M 16s
118250K .......... .......... .......... .......... .......... 45% 21.2M 16s
118300K .......... .......... .......... .......... .......... 45% 20.7M 16s
118350K .......... .......... .......... .......... .......... 45% 16.9M 16s
118400K .......... .......... .......... .......... .......... 45% 22.7M 16s
118450K .......... .......... .......... .......... .......... 45% 14.0M 16s
118500K .......... .......... .......... .......... .......... 45% 18.0M 16s
118550K .......... .......... .......... .......... .......... 45% 15.5M 16s
118600K .......... .......... .......... .......... .......... 45% 18.7M 16s
118650K .......... .......... .......... .......... .......... 45% 15.6M 16s
118700K .......... .......... .......... .......... .......... 45% 17.9M 16s
118750K .......... .......... .......... .......... .......... 45% 17.6M 16s
118800K .......... .......... .......... .......... .......... 45% 51.7M 16s
118850K .......... .......... .......... .......... .......... 45% 20.3M 16s
118900K .......... .......... .......... .......... .......... 45% 20.5M 16s
118950K .......... .......... .......... .......... .......... 45% 38.1M 16s
119000K .......... .......... .......... .......... .......... 45% 22.8M 16s
119050K .......... .......... .......... .......... .......... 45% 15.1M 16s
119100K .......... .......... .......... .......... .......... 45% 14.2M 16s
119150K .......... .......... .......... .......... .......... 45% 17.4M 16s
119200K .......... .......... .......... .......... .......... 45% 19.3M 16s
119250K .......... .......... .......... .......... .......... 45% 19.6M 16s
119300K .......... .......... .......... .......... .......... 45% 81.4M 16s
119350K .......... .......... .......... .......... .......... 45% 15.0M 16s
119400K .......... .......... .......... .......... .......... 45% 36.7M 16s
119450K .......... .......... .......... .......... .......... 45% 23.7M 16s
119500K .......... .......... .......... .......... .......... 45% 31.5M 16s
119550K .......... .......... .......... .......... .......... 45% 16.1M 16s
119600K .......... .......... .......... .......... .......... 45% 20.3M 16s
119650K .......... .......... .......... .......... .......... 45% 30.4M 16s
119700K .......... .......... .......... .......... .......... 45% 22.5M 16s
119750K .......... .......... .......... .......... .......... 45% 21.8M 16s
119800K .......... .......... .......... .......... .......... 45% 20.6M 16s
119850K .......... .......... .......... .......... .......... 45% 11.7M 16s
119900K .......... .......... .......... .......... .......... 45% 22.6M 16s
119950K .......... .......... .......... .......... .......... 45% 13.1M 16s
120000K .......... .......... .......... .......... .......... 45% 11.1M 16s
120050K .......... .......... .......... .......... .......... 45% 23.8M 16s
120100K .......... .......... .......... .......... .......... 45% 20.7M 16s
120150K .......... .......... .......... .......... .......... 45% 21.9M 16s
120200K .......... .......... .......... .......... .......... 45% 26.3M 16s
120250K .......... .......... .......... .......... .......... 45% 16.2M 16s
120300K .......... .......... .......... .......... .......... 45% 15.6M 16s
120350K .......... .......... .......... .......... .......... 45% 16.2M 16s
120400K .......... .......... .......... .......... .......... 45% 13.1M 16s
120450K .......... .......... .......... .......... .......... 45% 12.6M 16s
120500K .......... .......... .......... .......... .......... 45% 19.7M 16s
120550K .......... .......... .......... .......... .......... 45% 29.9M 16s
120600K .......... .......... .......... .......... .......... 46% 15.0M 16s
120650K .......... .......... .......... .......... .......... 46% 23.2M 16s
120700K .......... .......... .......... .......... .......... 46% 22.9M 16s
120750K .......... .......... .......... .......... .......... 46% 24.1M 16s
120800K .......... .......... .......... .......... .......... 46% 23.4M 16s
120850K .......... .......... .......... .......... .......... 46% 16.9M 16s
120900K .......... .......... .......... .......... .......... 46% 21.0M 16s
120950K .......... .......... .......... .......... .......... 46% 14.1M 16s
121000K .......... .......... .......... .......... .......... 46% 24.1M 16s
121050K .......... .......... .......... .......... .......... 46% 21.9M 16s
121100K .......... .......... .......... .......... .......... 46% 15.7M 16s
121150K .......... .......... .......... .......... .......... 46% 15.0M 16s
121200K .......... .......... .......... .......... .......... 46% 11.6M 16s
121250K .......... .......... .......... .......... .......... 46% 14.1M 16s
121300K .......... .......... .......... .......... .......... 46% 12.6M 16s
121350K .......... .......... .......... .......... .......... 46% 10.2M 16s
121400K .......... .......... .......... .......... .......... 46% 9.71M 16s
121450K .......... .......... .......... .......... .......... 46% 9.32M 16s
121500K .......... .......... .......... .......... .......... 46% 9.75M 16s
121550K .......... .......... .......... .......... .......... 46% 15.4M 16s
121600K .......... .......... .......... .......... .......... 46% 14.0M 16s
121650K .......... .......... .......... .......... .......... 46% 11.3M 16s
121700K .......... .......... .......... .......... .......... 46% 16.8M 16s
121750K .......... .......... .......... .......... .......... 46% 13.2M 16s
121800K .......... .......... .......... .......... .......... 46% 15.0M 16s
121850K .......... .......... .......... .......... .......... 46% 12.8M 16s
121900K .......... .......... .......... .......... .......... 46% 13.9M 16s
121950K .......... .......... .......... .......... .......... 46% 13.2M 16s
122000K .......... .......... .......... .......... .......... 46% 16.6M 16s
122050K .......... .......... .......... .......... .......... 46% 14.8M 16s
122100K .......... .......... .......... .......... .......... 46% 16.4M 16s
122150K .......... .......... .......... .......... .......... 46% 13.9M 16s
122200K .......... .......... .......... .......... .......... 46% 7.70M 16s
122250K .......... .......... .......... .......... .......... 46% 13.6M 16s
122300K .......... .......... .......... .......... .......... 46% 17.8M 16s
122350K .......... .......... .......... .......... .......... 46% 13.7M 16s
122400K .......... .......... .......... .......... .......... 46% 13.2M 16s
122450K .......... .......... .......... .......... .......... 46% 21.6M 16s
122500K .......... .......... .......... .......... .......... 46% 20.6M 16s
122550K .......... .......... .......... .......... .......... 46% 15.2M 16s
122600K .......... .......... .......... .......... .......... 46% 17.0M 16s
122650K .......... .......... .......... .......... .......... 46% 46.4M 16s
122700K .......... .......... .......... .......... .......... 46% 11.1M 16s
122750K .......... .......... .......... .......... .......... 46% 26.6M 16s
122800K .......... .......... .......... .......... .......... 46% 16.8M 16s
122850K .......... .......... .......... .......... .......... 46% 14.2M 16s
122900K .......... .......... .......... .......... .......... 46% 14.6M 16s
122950K .......... .......... .......... .......... .......... 46% 13.4M 16s
123000K .......... .......... .......... .......... .......... 46% 17.6M 16s
123050K .......... .......... .......... .......... .......... 46% 14.0M 16s
123100K .......... .......... .......... .......... .......... 46% 15.3M 16s
123150K .......... .......... .......... .......... .......... 46% 23.1M 16s
123200K .......... .......... .......... .......... .......... 47% 15.0M 16s
123250K .......... .......... .......... .......... .......... 47% 16.8M 16s
123300K .......... .......... .......... .......... .......... 47% 17.1M 16s
123350K .......... .......... .......... .......... .......... 47% 12.4M 16s
123400K .......... .......... .......... .......... .......... 47% 21.5M 16s
123450K .......... .......... .......... .......... .......... 47% 12.2M 16s
123500K .......... .......... .......... .......... .......... 47% 21.9M 16s
123550K .......... .......... .......... .......... .......... 47% 22.6M 16s
123600K .......... .......... .......... .......... .......... 47% 19.7M 15s
123650K .......... .......... .......... .......... .......... 47% 23.2M 15s
123700K .......... .......... .......... .......... .......... 47% 17.2M 15s
123750K .......... .......... .......... .......... .......... 47% 30.8M 15s
123800K .......... .......... .......... .......... .......... 47% 27.5M 15s
123850K .......... .......... .......... .......... .......... 47% 22.3M 15s
123900K .......... .......... .......... .......... .......... 47% 29.1M 15s
123950K .......... .......... .......... .......... .......... 47% 26.1M 15s
124000K .......... .......... .......... .......... .......... 47% 21.7M 15s
124050K .......... .......... .......... .......... .......... 47% 40.0M 15s
124100K .......... .......... .......... .......... .......... 47% 27.2M 15s
124150K .......... .......... .......... .......... .......... 47% 39.2M 15s
124200K .......... .......... .......... .......... .......... 47% 24.1M 15s
124250K .......... .......... .......... .......... .......... 47% 30.2M 15s
124300K .......... .......... .......... .......... .......... 47% 32.8M 15s
124350K .......... .......... .......... .......... .......... 47% 19.1M 15s
124400K .......... .......... .......... .......... .......... 47% 42.1M 15s
124450K .......... .......... .......... .......... .......... 47% 21.1M 15s
124500K .......... .......... .......... .......... .......... 47% 24.7M 15s
124550K .......... .......... .......... .......... .......... 47% 32.5M 15s
124600K .......... .......... .......... .......... .......... 47% 21.8M 15s
124650K .......... .......... .......... .......... .......... 47% 15.7M 15s
124700K .......... .......... .......... .......... .......... 47% 15.2M 15s
124750K .......... .......... .......... .......... .......... 47% 8.62M 15s
124800K .......... .......... .......... .......... .......... 47% 10.8M 15s
124850K .......... .......... .......... .......... .......... 47% 8.24M 15s
124900K .......... .......... .......... .......... .......... 47% 12.4M 15s
124950K .......... .......... .......... .......... .......... 47% 8.94M 15s
125000K .......... .......... .......... .......... .......... 47% 9.57M 15s
125050K .......... .......... .......... .......... .......... 47% 8.48M 15s
125100K .......... .......... .......... .......... .......... 47% 14.7M 15s
125150K .......... .......... .......... .......... .......... 47% 33.5M 15s
125200K .......... .......... .......... .......... .......... 47% 23.0M 15s
125250K .......... .......... .......... .......... .......... 47% 31.3M 15s
125300K .......... .......... .......... .......... .......... 47% 28.5M 15s
125350K .......... .......... .......... .......... .......... 47% 19.4M 15s
125400K .......... .......... .......... .......... .......... 47% 27.0M 15s
125450K .......... .......... .......... .......... .......... 47% 13.7M 15s
125500K .......... .......... .......... .......... .......... 47% 16.4M 15s
125550K .......... .......... .......... .......... .......... 47% 14.9M 15s
125600K .......... .......... .......... .......... .......... 47% 14.6M 15s
125650K .......... .......... .......... .......... .......... 47% 15.9M 15s
125700K .......... .......... .......... .......... .......... 47% 12.8M 15s
125750K .......... .......... .......... .......... .......... 47% 17.2M 15s
125800K .......... .......... .......... .......... .......... 47% 13.6M 15s
125850K .......... .......... .......... .......... .......... 48% 14.3M 15s
125900K .......... .......... .......... .......... .......... 48% 21.0M 15s
125950K .......... .......... .......... .......... .......... 48% 12.8M 15s
126000K .......... .......... .......... .......... .......... 48% 17.5M 15s
126050K .......... .......... .......... .......... .......... 48% 16.9M 15s
126100K .......... .......... .......... .......... .......... 48% 13.8M 15s
126150K .......... .......... .......... .......... .......... 48% 5.40M 15s
126200K .......... .......... .......... .......... .......... 48%  146M 15s
126250K .......... .......... .......... .......... .......... 48% 31.7M 15s
126300K .......... .......... .......... .......... .......... 48% 14.4M 15s
126350K .......... .......... .......... .......... .......... 48% 15.4M 15s
126400K .......... .......... .......... .......... .......... 48% 19.4M 15s
126450K .......... .......... .......... .......... .......... 48% 16.3M 15s
126500K .......... .......... .......... .......... .......... 48% 21.2M 15s
126550K .......... .......... .......... .......... .......... 48% 19.5M 15s
126600K .......... .......... .......... .......... .......... 48% 11.5M 15s
126650K .......... .......... .......... .......... .......... 48% 9.39M 15s
126700K .......... .......... .......... .......... .......... 48% 10.5M 15s
126750K .......... .......... .......... .......... .......... 48% 14.4M 15s
126800K .......... .......... .......... .......... .......... 48% 15.5M 15s
126850K .......... .......... .......... .......... .......... 48% 13.5M 15s
126900K .......... .......... .......... .......... .......... 48% 11.1M 15s
126950K .......... .......... .......... .......... .......... 48% 9.66M 15s
127000K .......... .......... .......... .......... .......... 48% 7.78M 15s
127050K .......... .......... .......... .......... .......... 48% 14.6M 15s
127100K .......... .......... .......... .......... .......... 48% 12.1M 15s
127150K .......... .......... .......... .......... .......... 48% 7.93M 15s
127200K .......... .......... .......... .......... .......... 48% 9.60M 15s
127250K .......... .......... .......... .......... .......... 48% 11.1M 15s
127300K .......... .......... .......... .......... .......... 48% 19.7M 15s
127350K .......... .......... .......... .......... .......... 48% 16.0M 15s
127400K .......... .......... .......... .......... .......... 48% 8.23M 15s
127450K .......... .......... .......... .......... .......... 48% 6.71M 15s
127500K .......... .......... .......... .......... .......... 48% 11.0M 15s
127550K .......... .......... .......... .......... .......... 48% 13.4M 15s
127600K .......... .......... .......... .......... .......... 48% 10.6M 15s
127650K .......... .......... .......... .......... .......... 48% 15.3M 15s
127700K .......... .......... .......... .......... .......... 48% 15.0M 15s
127750K .......... .......... .......... .......... .......... 48% 25.9M 15s
127800K .......... .......... .......... .......... .......... 48% 11.7M 15s
127850K .......... .......... .......... .......... .......... 48% 19.7M 15s
127900K .......... .......... .......... .......... .......... 48% 12.0M 15s
127950K .......... .......... .......... .......... .......... 48% 13.1M 15s
128000K .......... .......... .......... .......... .......... 48% 10.0M 15s
128050K .......... .......... .......... .......... .......... 48% 7.64M 15s
128100K .......... .......... .......... .......... .......... 48% 6.02M 15s
128150K .......... .......... .......... .......... .......... 48% 9.17M 15s
128200K .......... .......... .......... .......... .......... 48% 16.2M 15s
128250K .......... .......... .......... .......... .......... 48% 9.81M 15s
128300K .......... .......... .......... .......... .......... 48% 9.69M 15s
128350K .......... .......... .......... .......... .......... 48% 7.71M 15s
128400K .......... .......... .......... .......... .......... 48% 9.09M 15s
128450K .......... .......... .......... .......... .......... 49% 8.09M 15s
128500K .......... .......... .......... .......... .......... 49% 17.6M 15s
128550K .......... .......... .......... .......... .......... 49% 12.3M 15s
128600K .......... .......... .......... .......... .......... 49% 14.6M 15s
128650K .......... .......... .......... .......... .......... 49% 15.1M 15s
128700K .......... .......... .......... .......... .......... 49% 12.8M 15s
128750K .......... .......... .......... .......... .......... 49% 17.8M 15s
128800K .......... .......... .......... .......... .......... 49% 11.4M 15s
128850K .......... .......... .......... .......... .......... 49% 9.70M 15s
128900K .......... .......... .......... .......... .......... 49% 12.0M 15s
128950K .......... .......... .......... .......... .......... 49% 13.9M 15s
129000K .......... .......... .......... .......... .......... 49% 14.0M 15s
129050K .......... .......... .......... .......... .......... 49% 22.7M 15s
129100K .......... .......... .......... .......... .......... 49% 19.4M 15s
129150K .......... .......... .......... .......... .......... 49% 25.1M 15s
129200K .......... .......... .......... .......... .......... 49% 11.8M 15s
129250K .......... .......... .......... .......... .......... 49% 24.8M 15s
129300K .......... .......... .......... .......... .......... 49% 14.0M 15s
129350K .......... .......... .......... .......... .......... 49% 13.2M 15s
129400K .......... .......... .......... .......... .......... 49% 21.8M 15s
129450K .......... .......... .......... .......... .......... 49% 16.3M 15s
129500K .......... .......... .......... .......... .......... 49% 24.1M 15s
129550K .......... .......... .......... .......... .......... 49% 37.6M 15s
129600K .......... .......... .......... .......... .......... 49% 14.1M 15s
129650K .......... .......... .......... .......... .......... 49% 20.9M 15s
129700K .......... .......... .......... .......... .......... 49% 13.2M 15s
129750K .......... .......... .......... .......... .......... 49% 27.2M 15s
129800K .......... .......... .......... .......... .......... 49% 29.4M 15s
129850K .......... .......... .......... .......... .......... 49% 17.7M 15s
129900K .......... .......... .......... .......... .......... 49% 18.8M 15s
129950K .......... .......... .......... .......... .......... 49% 14.9M 15s
130000K .......... .......... .......... .......... .......... 49% 17.6M 14s
130050K .......... .......... .......... .......... .......... 49% 12.8M 14s
130100K .......... .......... .......... .......... .......... 49% 9.30M 14s
130150K .......... .......... .......... .......... .......... 49% 8.06M 14s
130200K .......... .......... .......... .......... .......... 49% 9.57M 14s
130250K .......... .......... .......... .......... .......... 49% 10.8M 14s
130300K .......... .......... .......... .......... .......... 49% 13.9M 14s
130350K .......... .......... .......... .......... .......... 49% 14.0M 14s
130400K .......... .......... .......... .......... .......... 49% 12.7M 14s
130450K .......... .......... .......... .......... .......... 49% 15.3M 14s
130500K .......... .......... .......... .......... .......... 49% 8.75M 14s
130550K .......... .......... .......... .......... .......... 49% 8.58M 14s
130600K .......... .......... .......... .......... .......... 49% 8.27M 14s
130650K .......... .......... .......... .......... .......... 49% 8.99M 14s
130700K .......... .......... .......... .......... .......... 49% 20.8M 14s
130750K .......... .......... .......... .......... .......... 49% 18.2M 14s
130800K .......... .......... .......... .......... .......... 49% 19.1M 14s
130850K .......... .......... .......... .......... .......... 49% 17.4M 14s
130900K .......... .......... .......... .......... .......... 49% 15.6M 14s
130950K .......... .......... .......... .......... .......... 49% 13.5M 14s
131000K .......... .......... .......... .......... .......... 49% 11.3M 14s
131050K .......... .......... .......... .......... .......... 50% 13.4M 14s
131100K .......... .......... .......... .......... .......... 50% 10.5M 14s
131150K .......... .......... .......... .......... .......... 50% 24.3M 14s
131200K .......... .......... .......... .......... .......... 50% 8.47M 14s
131250K .......... .......... .......... .......... .......... 50% 13.3M 14s
131300K .......... .......... .......... .......... .......... 50% 11.9M 14s
131350K .......... .......... .......... .......... .......... 50% 9.64M 14s
131400K .......... .......... .......... .......... .......... 50% 10.8M 14s
131450K .......... .......... .......... .......... .......... 50% 10.9M 14s
131500K .......... .......... .......... .......... .......... 50% 20.6M 14s
131550K .......... .......... .......... .......... .......... 50% 25.2M 14s
131600K .......... .......... .......... .......... .......... 50% 19.6M 14s
131650K .......... .......... .......... .......... .......... 50% 9.96M 14s
131700K .......... .......... .......... .......... .......... 50% 19.4M 14s
131750K .......... .......... .......... .......... .......... 50% 14.7M 14s
131800K .......... .......... .......... .......... .......... 50% 17.0M 14s
131850K .......... .......... .......... .......... .......... 50% 14.9M 14s
131900K .......... .......... .......... .......... .......... 50% 25.9M 14s
131950K .......... .......... .......... .......... .......... 50% 14.9M 14s
132000K .......... .......... .......... .......... .......... 50% 22.6M 14s
132050K .......... .......... .......... .......... .......... 50% 18.1M 14s
132100K .......... .......... .......... .......... .......... 50% 17.6M 14s
132150K .......... .......... .......... .......... .......... 50% 17.1M 14s
132200K .......... .......... .......... .......... .......... 50% 18.2M 14s
132250K .......... .......... .......... .......... .......... 50% 13.0M 14s
132300K .......... .......... .......... .......... .......... 50% 17.3M 14s
132350K .......... .......... .......... .......... .......... 50% 12.2M 14s
132400K .......... .......... .......... .......... .......... 50% 16.7M 14s
132450K .......... .......... .......... .......... .......... 50% 16.2M 14s
132500K .......... .......... .......... .......... .......... 50% 22.7M 14s
132550K .......... .......... .......... .......... .......... 50% 13.2M 14s
132600K .......... .......... .......... .......... .......... 50% 8.53M 14s
132650K .......... .......... .......... .......... .......... 50% 19.3M 14s
132700K .......... .......... .......... .......... .......... 50% 14.8M 14s
132750K .......... .......... .......... .......... .......... 50% 15.0M 14s
132800K .......... .......... .......... .......... .......... 50% 15.3M 14s
132850K .......... .......... .......... .......... .......... 50% 10.5M 14s
132900K .......... .......... .......... .......... .......... 50% 15.3M 14s
132950K .......... .......... .......... .......... .......... 50% 12.9M 14s
133000K .......... .......... .......... .......... .......... 50% 11.5M 14s
133050K .......... .......... .......... .......... .......... 50% 23.3M 14s
133100K .......... .......... .......... .......... .......... 50% 15.7M 14s
133150K .......... .......... .......... .......... .......... 50% 26.8M 14s
133200K .......... .......... .......... .......... .......... 50% 21.4M 14s
133250K .......... .......... .......... .......... .......... 50% 28.2M 14s
133300K .......... .......... .......... .......... .......... 50% 20.9M 14s
133350K .......... .......... .......... .......... .......... 50% 20.0M 14s
133400K .......... .......... .......... .......... .......... 50% 18.5M 14s
133450K .......... .......... .......... .......... .......... 50% 19.3M 14s
133500K .......... .......... .......... .......... .......... 50% 25.0M 14s
133550K .......... .......... .......... .......... .......... 50% 42.0M 14s
133600K .......... .......... .......... .......... .......... 50% 22.3M 14s
133650K .......... .......... .......... .......... .......... 50% 19.5M 14s
133700K .......... .......... .......... .......... .......... 51% 15.9M 14s
133750K .......... .......... .......... .......... .......... 51% 18.1M 14s
133800K .......... .......... .......... .......... .......... 51% 22.9M 14s
133850K .......... .......... .......... .......... .......... 51% 11.5M 14s
133900K .......... .......... .......... .......... .......... 51% 8.20M 14s
133950K .......... .......... .......... .......... .......... 51% 18.8M 14s
134000K .......... .......... .......... .......... .......... 51% 18.5M 14s
134050K .......... .......... .......... .......... .......... 51% 14.5M 14s
134100K .......... .......... .......... .......... .......... 51% 9.07M 14s
134150K .......... .......... .......... .......... .......... 51% 13.0M 14s
134200K .......... .......... .......... .......... .......... 51% 8.03M 14s
134250K .......... .......... .......... .......... .......... 51% 12.8M 14s
134300K .......... .......... .......... .......... .......... 51% 11.0M 14s
134350K .......... .......... .......... .......... .......... 51% 7.76M 14s
134400K .......... .......... .......... .......... .......... 51% 10.6M 14s
134450K .......... .......... .......... .......... .......... 51% 10.6M 14s
134500K .......... .......... .......... .......... .......... 51% 14.7M 14s
134550K .......... .......... .......... .......... .......... 51% 17.4M 14s
134600K .......... .......... .......... .......... .......... 51% 8.45M 14s
134650K .......... .......... .......... .......... .......... 51% 10.6M 14s
134700K .......... .......... .......... .......... .......... 51% 9.45M 14s
134750K .......... .......... .......... .......... .......... 51% 13.2M 14s
134800K .......... .......... .......... .......... .......... 51% 15.6M 14s
134850K .......... .......... .......... .......... .......... 51% 10.6M 14s
134900K .......... .......... .......... .......... .......... 51% 13.3M 14s
134950K .......... .......... .......... .......... .......... 51% 15.6M 14s
135000K .......... .......... .......... .......... .......... 51% 19.5M 14s
135050K .......... .......... .......... .......... .......... 51% 29.7M 14s
135100K .......... .......... .......... .......... .......... 51% 14.8M 14s
135150K .......... .......... .......... .......... .......... 51% 30.1M 14s
135200K .......... .......... .......... .......... .......... 51% 11.6M 14s
135250K .......... .......... .......... .......... .......... 51% 13.9M 14s
135300K .......... .......... .......... .......... .......... 51% 24.4M 14s
135350K .......... .......... .......... .......... .......... 51% 13.6M 14s
135400K .......... .......... .......... .......... .......... 51% 15.3M 14s
135450K .......... .......... .......... .......... .......... 51% 9.42M 14s
135500K .......... .......... .......... .......... .......... 51% 10.3M 14s
135550K .......... .......... .......... .......... .......... 51% 13.7M 14s
135600K .......... .......... .......... .......... .......... 51% 13.9M 14s
135650K .......... .......... .......... .......... .......... 51% 15.8M 14s
135700K .......... .......... .......... .......... .......... 51% 18.9M 14s
135750K .......... .......... .......... .......... .......... 51% 18.6M 14s
135800K .......... .......... .......... .......... .......... 51% 23.9M 14s
135850K .......... .......... .......... .......... .......... 51% 21.0M 14s
135900K .......... .......... .......... .......... .......... 51% 20.4M 14s
135950K .......... .......... .......... .......... .......... 51% 21.5M 14s
136000K .......... .......... .......... .......... .......... 51% 19.6M 14s
136050K .......... .......... .......... .......... .......... 51% 15.7M 14s
136100K .......... .......... .......... .......... .......... 51% 14.8M 14s
136150K .......... .......... .......... .......... .......... 51% 21.7M 14s
136200K .......... .......... .......... .......... .......... 51% 21.6M 14s
136250K .......... .......... .......... .......... .......... 51% 17.9M 14s
136300K .......... .......... .......... .......... .......... 52% 24.3M 14s
136350K .......... .......... .......... .......... .......... 52% 24.3M 14s
136400K .......... .......... .......... .......... .......... 52% 24.1M 14s
136450K .......... .......... .......... .......... .......... 52% 24.4M 14s
136500K .......... .......... .......... .......... .......... 52% 20.5M 14s
136550K .......... .......... .......... .......... .......... 52% 30.7M 14s
136600K .......... .......... .......... .......... .......... 52% 14.3M 14s
136650K .......... .......... .......... .......... .......... 52% 18.7M 14s
136700K .......... .......... .......... .......... .......... 52% 10.7M 14s
136750K .......... .......... .......... .......... .......... 52% 18.1M 13s
136800K .......... .......... .......... .......... .......... 52% 13.0M 13s
136850K .......... .......... .......... .......... .......... 52% 10.1M 13s
136900K .......... .......... .......... .......... .......... 52% 16.7M 13s
136950K .......... .......... .......... .......... .......... 52% 10.3M 13s
137000K .......... .......... .......... .......... .......... 52% 13.9M 13s
137050K .......... .......... .......... .......... .......... 52% 8.96M 13s
137100K .......... .......... .......... .......... .......... 52% 9.44M 13s
137150K .......... .......... .......... .......... .......... 52% 8.61M 13s
137200K .......... .......... .......... .......... .......... 52% 7.42M 13s
137250K .......... .......... .......... .......... .......... 52% 10.9M 13s
137300K .......... .......... .......... .......... .......... 52% 11.2M 13s
137350K .......... .......... .......... .......... .......... 52% 12.8M 13s
137400K .......... .......... .......... .......... .......... 52% 15.2M 13s
137450K .......... .......... .......... .......... .......... 52% 18.2M 13s
137500K .......... .......... .......... .......... .......... 52% 16.0M 13s
137550K .......... .......... .......... .......... .......... 52% 11.8M 13s
137600K .......... .......... .......... .......... .......... 52% 10.2M 13s
137650K .......... .......... .......... .......... .......... 52% 16.4M 13s
137700K .......... .......... .......... .......... .......... 52% 18.0M 13s
137750K .......... .......... .......... .......... .......... 52% 29.5M 13s
137800K .......... .......... .......... .......... .......... 52% 11.4M 13s
137850K .......... .......... .......... .......... .......... 52% 14.7M 13s
137900K .......... .......... .......... .......... .......... 52% 15.3M 13s
137950K .......... .......... .......... .......... .......... 52% 9.95M 13s
138000K .......... .......... .......... .......... .......... 52% 16.1M 13s
138050K .......... .......... .......... .......... .......... 52% 20.6M 13s
138100K .......... .......... .......... .......... .......... 52% 18.6M 13s
138150K .......... .......... .......... .......... .......... 52% 16.7M 13s
138200K .......... .......... .......... .......... .......... 52% 21.0M 13s
138250K .......... .......... .......... .......... .......... 52% 21.2M 13s
138300K .......... .......... .......... .......... .......... 52% 23.6M 13s
138350K .......... .......... .......... .......... .......... 52% 18.5M 13s
138400K .......... .......... .......... .......... .......... 52% 17.8M 13s
138450K .......... .......... .......... .......... .......... 52% 18.1M 13s
138500K .......... .......... .......... .......... .......... 52% 19.7M 13s
138550K .......... .......... .......... .......... .......... 52% 18.7M 13s
138600K .......... .......... .......... .......... .......... 52% 12.6M 13s
138650K .......... .......... .......... .......... .......... 52% 18.9M 13s
138700K .......... .......... .......... .......... .......... 52% 13.1M 13s
138750K .......... .......... .......... .......... .......... 52% 14.7M 13s
138800K .......... .......... .......... .......... .......... 52% 2.54M 13s
138850K .......... .......... .......... .......... .......... 52% 13.8M 13s
138900K .......... .......... .......... .......... .......... 52% 15.7M 13s
138950K .......... .......... .......... .......... .......... 53% 18.8M 13s
139000K .......... .......... .......... .......... .......... 53% 16.7M 13s
139050K .......... .......... .......... .......... .......... 53% 17.5M 13s
139100K .......... .......... .......... .......... .......... 53% 13.3M 13s
139150K .......... .......... .......... .......... .......... 53% 10.3M 13s
139200K .......... .......... .......... .......... .......... 53% 9.04M 13s
139250K .......... .......... .......... .......... .......... 53% 7.52M 13s
139300K .......... .......... .......... .......... .......... 53% 8.47M 13s
139350K .......... .......... .......... .......... .......... 53% 12.3M 13s
139400K .......... .......... .......... .......... .......... 53% 26.1M 13s
139450K .......... .......... .......... .......... .......... 53% 12.2M 13s
139500K .......... .......... .......... .......... .......... 53% 21.0M 13s
139550K .......... .......... .......... .......... .......... 53% 14.5M 13s
139600K .......... .......... .......... .......... .......... 53% 13.5M 13s
139650K .......... .......... .......... .......... .......... 53% 12.3M 13s
139700K .......... .......... .......... .......... .......... 53% 18.3M 13s
139750K .......... .......... .......... .......... .......... 53% 20.3M 13s
139800K .......... .......... .......... .......... .......... 53% 33.8M 13s
139850K .......... .......... .......... .......... .......... 53% 22.8M 13s
139900K .......... .......... .......... .......... .......... 53% 21.9M 13s
139950K .......... .......... .......... .......... .......... 53% 28.7M 13s
140000K .......... .......... .......... .......... .......... 53% 23.1M 13s
140050K .......... .......... .......... .......... .......... 53% 19.1M 13s
140100K .......... .......... .......... .......... .......... 53% 20.7M 13s
140150K .......... .......... .......... .......... .......... 53% 16.5M 13s
140200K .......... .......... .......... .......... .......... 53% 13.9M 13s
140250K .......... .......... .......... .......... .......... 53% 16.9M 13s
140300K .......... .......... .......... .......... .......... 53% 23.2M 13s
140350K .......... .......... .......... .......... .......... 53% 19.0M 13s
140400K .......... .......... .......... .......... .......... 53% 17.2M 13s
140450K .......... .......... .......... .......... .......... 53% 23.4M 13s
140500K .......... .......... .......... .......... .......... 53% 14.2M 13s
140550K .......... .......... .......... .......... .......... 53% 16.3M 13s
140600K .......... .......... .......... .......... .......... 53% 9.88M 13s
140650K .......... .......... .......... .......... .......... 53% 8.44M 13s
140700K .......... .......... .......... .......... .......... 53% 11.5M 13s
140750K .......... .......... .......... .......... .......... 53% 10.8M 13s
140800K .......... .......... .......... .......... .......... 53% 7.83M 13s
140850K .......... .......... .......... .......... .......... 53% 8.86M 13s
140900K .......... .......... .......... .......... .......... 53% 9.24M 13s
140950K .......... .......... .......... .......... .......... 53% 9.81M 13s
141000K .......... .......... .......... .......... .......... 53% 11.4M 13s
141050K .......... .......... .......... .......... .......... 53% 8.51M 13s
141100K .......... .......... .......... .......... .......... 53% 8.03M 13s
141150K .......... .......... .......... .......... .......... 53% 6.39M 13s
141200K .......... .......... .......... .......... .......... 53% 10.2M 13s
141250K .......... .......... .......... .......... .......... 53% 10.9M 13s
141300K .......... .......... .......... .......... .......... 53% 12.0M 13s
141350K .......... .......... .......... .......... .......... 53% 9.11M 13s
141400K .......... .......... .......... .......... .......... 53% 13.1M 13s
141450K .......... .......... .......... .......... .......... 53% 13.0M 13s
141500K .......... .......... .......... .......... .......... 53% 16.5M 13s
141550K .......... .......... .......... .......... .......... 54% 19.5M 13s
141600K .......... .......... .......... .......... .......... 54% 18.2M 13s
141650K .......... .......... .......... .......... .......... 54% 22.9M 13s
141700K .......... .......... .......... .......... .......... 54% 20.3M 13s
141750K .......... .......... .......... .......... .......... 54% 19.9M 13s
141800K .......... .......... .......... .......... .......... 54% 20.3M 13s
141850K .......... .......... .......... .......... .......... 54% 19.6M 13s
141900K .......... .......... .......... .......... .......... 54% 18.2M 13s
141950K .......... .......... .......... .......... .......... 54% 19.1M 13s
142000K .......... .......... .......... .......... .......... 54% 23.1M 13s
142050K .......... .......... .......... .......... .......... 54% 20.6M 13s
142100K .......... .......... .......... .......... .......... 54% 17.9M 13s
142150K .......... .......... .......... .......... .......... 54% 16.4M 13s
142200K .......... .......... .......... .......... .......... 54% 12.8M 13s
142250K .......... .......... .......... .......... .......... 54% 14.3M 13s
142300K .......... .......... .......... .......... .......... 54% 11.8M 13s
142350K .......... .......... .......... .......... .......... 54% 10.9M 13s
142400K .......... .......... .......... .......... .......... 54% 8.80M 13s
142450K .......... .......... .......... .......... .......... 54% 6.68M 13s
142500K .......... .......... .......... .......... .......... 54% 28.6M 13s
142550K .......... .......... .......... .......... .......... 54% 20.8M 13s
142600K .......... .......... .......... .......... .......... 54% 14.8M 13s
142650K .......... .......... .......... .......... .......... 54% 18.3M 13s
142700K .......... .......... .......... .......... .......... 54% 16.7M 13s
142750K .......... .......... .......... .......... .......... 54% 15.2M 13s
142800K .......... .......... .......... .......... .......... 54% 16.8M 13s
142850K .......... .......... .......... .......... .......... 54% 12.8M 13s
142900K .......... .......... .......... .......... .......... 54% 13.5M 13s
142950K .......... .......... .......... .......... .......... 54% 20.3M 13s
143000K .......... .......... .......... .......... .......... 54% 12.4M 13s
143050K .......... .......... .......... .......... .......... 54% 18.3M 13s
143100K .......... .......... .......... .......... .......... 54% 19.5M 13s
143150K .......... .......... .......... .......... .......... 54% 21.2M 13s
143200K .......... .......... .......... .......... .......... 54% 15.7M 13s
143250K .......... .......... .......... .......... .......... 54% 32.6M 13s
143300K .......... .......... .......... .......... .......... 54% 20.8M 13s
143350K .......... .......... .......... .......... .......... 54% 19.8M 13s
143400K .......... .......... .......... .......... .......... 54% 34.5M 13s
143450K .......... .......... .......... .......... .......... 54% 16.5M 13s
143500K .......... .......... .......... .......... .......... 54% 37.1M 13s
143550K .......... .......... .......... .......... .......... 54% 26.4M 13s
143600K .......... .......... .......... .......... .......... 54% 17.6M 13s
143650K .......... .......... .......... .......... .......... 54% 29.5M 13s
143700K .......... .......... .......... .......... .......... 54% 29.4M 13s
143750K .......... .......... .......... .......... .......... 54% 29.6M 13s
143800K .......... .......... .......... .......... .......... 54% 27.4M 13s
143850K .......... .......... .......... .......... .......... 54% 21.3M 13s
143900K .......... .......... .......... .......... .......... 54% 22.2M 12s
143950K .......... .......... .......... .......... .......... 54% 15.5M 12s
144000K .......... .......... .......... .......... .......... 54% 15.6M 12s
144050K .......... .......... .......... .......... .......... 54% 12.4M 12s
144100K .......... .......... .......... .......... .......... 54% 13.8M 12s
144150K .......... .......... .......... .......... .......... 54% 14.1M 12s
144200K .......... .......... .......... .......... .......... 55%  720K 13s
144250K .......... .......... .......... .......... .......... 55% 1.30M 13s
144300K .......... .......... .......... .......... .......... 55% 3.23M 13s
144350K .......... .......... .......... .......... .......... 55% 3.36M 13s
144400K .......... .......... .......... .......... .......... 55% 75.7K 13s
144450K .......... .......... .......... .......... .......... 55% 3.24M 13s
144500K .......... .......... .......... .......... .......... 55% 3.65M 13s
144550K .......... .......... .......... .......... .......... 55% 5.24M 13s
144600K .......... .......... .......... .......... .......... 55% 4.61M 13s
144650K .......... .......... .......... .......... .......... 55% 18.1M 13s
144700K .......... .......... .......... .......... .......... 55% 14.6M 13s
144750K .......... .......... .......... .......... .......... 55% 11.5M 13s
144800K .......... .......... .......... .......... .......... 55% 9.65M 13s
144850K .......... .......... .......... .......... .......... 55% 9.63M 13s
144900K .......... .......... .......... .......... .......... 55% 9.57M 13s
144950K .......... .......... .......... .......... .......... 55% 7.18M 13s
145000K .......... .......... .......... .......... .......... 55% 22.9M 13s
145050K .......... .......... .......... .......... .......... 55% 12.5M 13s
145100K .......... .......... .......... .......... .......... 55% 68.4M 13s
145150K .......... .......... .......... .......... .......... 55% 15.9M 13s
145200K .......... .......... .......... .......... .......... 55% 13.3M 13s
145250K .......... .......... .......... .......... .......... 55% 18.5M 13s
145300K .......... .......... .......... .......... .......... 55% 22.8M 13s
145350K .......... .......... .......... .......... .......... 55% 12.1M 13s
145400K .......... .......... .......... .......... .......... 55% 19.2M 13s
145450K .......... .......... .......... .......... .......... 55% 8.97M 13s
145500K .......... .......... .......... .......... .......... 55% 18.5M 13s
145550K .......... .......... .......... .......... .......... 55% 19.4M 13s
145600K .......... .......... .......... .......... .......... 55% 15.2M 13s
145650K .......... .......... .......... .......... .......... 55% 12.3M 13s
145700K .......... .......... .......... .......... .......... 55% 14.3M 13s
145750K .......... .......... .......... .......... .......... 55% 18.5M 13s
145800K .......... .......... .......... .......... .......... 55% 7.29M 13s
145850K .......... .......... .......... .......... .......... 55% 11.0M 13s
145900K .......... .......... .......... .......... .......... 55% 7.57M 13s
145950K .......... .......... .......... .......... .......... 55% 18.2M 13s
146000K .......... .......... .......... .......... .......... 55% 10.5M 13s
146050K .......... .......... .......... .......... .......... 55% 9.47M 13s
146100K .......... .......... .......... .......... .......... 55% 12.8M 13s
146150K .......... .......... .......... .......... .......... 55% 28.1M 13s
146200K .......... .......... .......... .......... .......... 55% 30.2M 13s
146250K .......... .......... .......... .......... .......... 55% 18.3M 13s
146300K .......... .......... .......... .......... .......... 55% 18.0M 13s
146350K .......... .......... .......... .......... .......... 55% 28.1M 13s
146400K .......... .......... .......... .......... .......... 55% 20.2M 13s
146450K .......... .......... .......... .......... .......... 55% 14.3M 13s
146500K .......... .......... .......... .......... .......... 55% 21.4M 13s
146550K .......... .......... .......... .......... .......... 55% 27.4M 13s
146600K .......... .......... .......... .......... .......... 55% 15.8M 13s
146650K .......... .......... .......... .......... .......... 55% 18.7M 13s
146700K .......... .......... .......... .......... .......... 55% 21.2M 13s
146750K .......... .......... .......... .......... .......... 55% 12.0M 13s
146800K .......... .......... .......... .......... .......... 56% 17.1M 13s
146850K .......... .......... .......... .......... .......... 56% 17.6M 13s
146900K .......... .......... .......... .......... .......... 56% 17.7M 13s
146950K .......... .......... .......... .......... .......... 56% 15.4M 13s
147000K .......... .......... .......... .......... .......... 56% 13.3M 13s
147050K .......... .......... .......... .......... .......... 56% 12.9M 13s
147100K .......... .......... .......... .......... .......... 56% 5.94M 13s
147150K .......... .......... .......... .......... .......... 56% 1.89M 13s
147200K .......... .......... .......... .......... .......... 56% 1.39M 13s
147250K .......... .......... .......... .......... .......... 56% 1.14M 13s
147300K .......... .......... .......... .......... .......... 56% 1.91M 13s
147350K .......... .......... .......... .......... .......... 56% 1.10M 13s
147400K .......... .......... .......... .......... .......... 56% 2.01M 13s
147450K .......... .......... .......... .......... .......... 56% 3.73M 13s
147500K .......... .......... .......... .......... .......... 56% 4.58M 13s
147550K .......... .......... .......... .......... .......... 56% 2.08M 13s
147600K .......... .......... .......... .......... .......... 56% 1.51M 13s
147650K .......... .......... .......... .......... .......... 56% 1.27M 13s
147700K .......... .......... .......... .......... .......... 56% 1.68M 13s
147750K .......... .......... .......... .......... .......... 56% 1.08M 13s
147800K .......... .......... .......... .......... .......... 56% 3.46M 13s
147850K .......... .......... .......... .......... .......... 56% 1.53M 13s
147900K .......... .......... .......... .......... .......... 56% 1.76M 13s
147950K .......... .......... .......... .......... .......... 56% 1.01M 13s
148000K .......... .......... .......... .......... .......... 56% 1.06M 13s
148050K .......... .......... .......... .......... .......... 56% 3.78M 13s
148100K .......... .......... .......... .......... .......... 56% 1.72M 13s
148150K .......... .......... .......... .......... .......... 56%  209K 13s
148200K .......... .......... .......... .......... .......... 56% 5.08M 13s
148250K .......... .......... .......... .......... .......... 56% 11.3M 13s
148300K .......... .......... .......... .......... .......... 56% 9.30M 13s
148350K .......... .......... .......... .......... .......... 56% 9.96M 13s
148400K .......... .......... .......... .......... .......... 56% 10.5M 13s
148450K .......... .......... .......... .......... .......... 56% 10.2M 13s
148500K .......... .......... .......... .......... .......... 56% 31.4M 13s
148550K .......... .......... .......... .......... .......... 56% 18.3M 13s
148600K .......... .......... .......... .......... .......... 56% 12.5M 13s
148650K .......... .......... .......... .......... .......... 56% 15.3M 13s
148700K .......... .......... .......... .......... .......... 56% 19.6M 13s
148750K .......... .......... .......... .......... .......... 56% 14.3M 13s
148800K .......... .......... .......... .......... .......... 56% 21.0M 13s
148850K .......... .......... .......... .......... .......... 56% 14.5M 13s
148900K .......... .......... .......... .......... .......... 56% 18.3M 13s
148950K .......... .......... .......... .......... .......... 56% 13.8M 13s
149000K .......... .......... .......... .......... .......... 56% 18.9M 13s
149050K .......... .......... .......... .......... .......... 56% 12.9M 13s
149100K .......... .......... .......... .......... .......... 56% 10.4M 13s
149150K .......... .......... .......... .......... .......... 56% 15.6M 13s
149200K .......... .......... .......... .......... .......... 56% 9.29M 13s
149250K .......... .......... .......... .......... .......... 56% 15.9M 13s
149300K .......... .......... .......... .......... .......... 56% 18.1M 13s
149350K .......... .......... .......... .......... .......... 56% 11.9M 13s
149400K .......... .......... .......... .......... .......... 56% 20.2M 13s
149450K .......... .......... .......... .......... .......... 57% 16.0M 13s
149500K .......... .......... .......... .......... .......... 57% 39.1M 13s
149550K .......... .......... .......... .......... .......... 57% 24.9M 13s
149600K .......... .......... .......... .......... .......... 57% 19.9M 13s
149650K .......... .......... .......... .......... .......... 57% 18.3M 13s
149700K .......... .......... .......... .......... .......... 57% 17.5M 13s
149750K .......... .......... .......... .......... .......... 57% 18.9M 13s
149800K .......... .......... .......... .......... .......... 57% 14.7M 13s
149850K .......... .......... .......... .......... .......... 57% 11.8M 13s
149900K .......... .......... .......... .......... .......... 57% 12.4M 13s
149950K .......... .......... .......... .......... .......... 57% 14.5M 13s
150000K .......... .......... .......... .......... .......... 57% 19.5M 13s
150050K .......... .......... .......... .......... .......... 57% 8.89M 13s
150100K .......... .......... .......... .......... .......... 57% 11.7M 13s
150150K .......... .......... .......... .......... .......... 57% 10.6M 13s
150200K .......... .......... .......... .......... .......... 57% 15.8M 13s
150250K .......... .......... .......... .......... .......... 57% 14.8M 13s
150300K .......... .......... .......... .......... .......... 57% 21.2M 13s
150350K .......... .......... .......... .......... .......... 57% 11.5M 13s
150400K .......... .......... .......... .......... .......... 57% 15.2M 13s
150450K .......... .......... .......... .......... .......... 57% 15.8M 13s
150500K .......... .......... .......... .......... .......... 57% 20.8M 13s
150550K .......... .......... .......... .......... .......... 57% 19.6M 13s
150600K .......... .......... .......... .......... .......... 57% 19.5M 13s
150650K .......... .......... .......... .......... .......... 57% 16.2M 13s
150700K .......... .......... .......... .......... .......... 57% 14.6M 13s
150750K .......... .......... .......... .......... .......... 57% 20.5M 13s
150800K .......... .......... .......... .......... .......... 57% 14.9M 13s
150850K .......... .......... .......... .......... .......... 57% 14.0M 13s
150900K .......... .......... .......... .......... .......... 57% 13.5M 13s
150950K .......... .......... .......... .......... .......... 57% 12.8M 13s
151000K .......... .......... .......... .......... .......... 57% 13.0M 13s
151050K .......... .......... .......... .......... .......... 57% 20.8M 13s
151100K .......... .......... .......... .......... .......... 57% 13.0M 13s
151150K .......... .......... .......... .......... .......... 57% 20.4M 13s
151200K .......... .......... .......... .......... .......... 57% 15.4M 13s
151250K .......... .......... .......... .......... .......... 57% 14.8M 13s
151300K .......... .......... .......... .......... .......... 57% 15.2M 13s
151350K .......... .......... .......... .......... .......... 57% 12.2M 13s
151400K .......... .......... .......... .......... .......... 57% 13.3M 13s
151450K .......... .......... .......... .......... .......... 57% 9.12M 13s
151500K .......... .......... .......... .......... .......... 57% 9.40M 13s
151550K .......... .......... .......... .......... .......... 57% 9.86M 13s
151600K .......... .......... .......... .......... .......... 57% 14.6M 13s
151650K .......... .......... .......... .......... .......... 57% 18.2M 13s
151700K .......... .......... .......... .......... .......... 57% 16.9M 13s
151750K .......... .......... .......... .......... .......... 57% 22.2M 13s
151800K .......... .......... .......... .......... .......... 57% 30.3M 13s
151850K .......... .......... .......... .......... .......... 57% 22.2M 13s
151900K .......... .......... .......... .......... .......... 57% 21.0M 13s
151950K .......... .......... .......... .......... .......... 57% 18.7M 13s
152000K .......... .......... .......... .......... .......... 57% 18.4M 13s
152050K .......... .......... .......... .......... .......... 58% 18.3M 13s
152100K .......... .......... .......... .......... .......... 58% 11.3M 13s
152150K .......... .......... .......... .......... .......... 58% 16.3M 13s
152200K .......... .......... .......... .......... .......... 58% 13.4M 13s
152250K .......... .......... .......... .......... .......... 58% 13.6M 13s
152300K .......... .......... .......... .......... .......... 58% 11.4M 13s
152350K .......... .......... .......... .......... .......... 58% 11.0M 13s
152400K .......... .......... .......... .......... .......... 58% 9.49M 13s
152450K .......... .......... .......... .......... .......... 58% 9.05M 13s
152500K .......... .......... .......... .......... .......... 58% 9.45M 13s
152550K .......... .......... .......... .......... .......... 58% 7.26M 12s
152600K .......... .......... .......... .......... .......... 58% 9.28M 12s
152650K .......... .......... .......... .......... .......... 58% 10.3M 12s
152700K .......... .......... .......... .......... .......... 58% 8.81M 12s
152750K .......... .......... .......... .......... .......... 58% 12.8M 12s
152800K .......... .......... .......... .......... .......... 58% 14.2M 12s
152850K .......... .......... .......... .......... .......... 58% 13.1M 12s
152900K .......... .......... .......... .......... .......... 58% 15.5M 12s
152950K .......... .......... .......... .......... .......... 58% 14.5M 12s
153000K .......... .......... .......... .......... .......... 58% 14.7M 12s
153050K .......... .......... .......... .......... .......... 58% 20.8M 12s
153100K .......... .......... .......... .......... .......... 58% 18.0M 12s
153150K .......... .......... .......... .......... .......... 58% 14.1M 12s
153200K .......... .......... .......... .......... .......... 58% 19.4M 12s
153250K .......... .......... .......... .......... .......... 58% 17.7M 12s
153300K .......... .......... .......... .......... .......... 58% 19.4M 12s
153350K .......... .......... .......... .......... .......... 58% 15.7M 12s
153400K .......... .......... .......... .......... .......... 58% 20.6M 12s
153450K .......... .......... .......... .......... .......... 58% 14.1M 12s
153500K .......... .......... .......... .......... .......... 58% 24.7M 12s
153550K .......... .......... .......... .......... .......... 58% 17.5M 12s
153600K .......... .......... .......... .......... .......... 58% 18.2M 12s
153650K .......... .......... .......... .......... .......... 58% 26.4M 12s
153700K .......... .......... .......... .......... .......... 58% 14.7M 12s
153750K .......... .......... .......... .......... .......... 58% 24.4M 12s
153800K .......... .......... .......... .......... .......... 58% 17.6M 12s
153850K .......... .......... .......... .......... .......... 58% 23.3M 12s
153900K .......... .......... .......... .......... .......... 58% 19.4M 12s
153950K .......... .......... .......... .......... .......... 58% 12.5M 12s
154000K .......... .......... .......... .......... .......... 58% 13.1M 12s
154050K .......... .......... .......... .......... .......... 58% 14.2M 12s
154100K .......... .......... .......... .......... .......... 58% 12.5M 12s
154150K .......... .......... .......... .......... .......... 58% 19.1M 12s
154200K .......... .......... .......... .......... .......... 58% 14.6M 12s
154250K .......... .......... .......... .......... .......... 58% 12.5M 12s
154300K .......... .......... .......... .......... .......... 58% 17.7M 12s
154350K .......... .......... .......... .......... .......... 58% 12.9M 12s
154400K .......... .......... .......... .......... .......... 58% 9.21M 12s
154450K .......... .......... .......... .......... .......... 58% 12.4M 12s
154500K .......... .......... .......... .......... .......... 58% 10.5M 12s
154550K .......... .......... .......... .......... .......... 58% 12.5M 12s
154600K .......... .......... .......... .......... .......... 58% 12.7M 12s
154650K .......... .......... .......... .......... .......... 59% 14.6M 12s
154700K .......... .......... .......... .......... .......... 59% 9.75M 12s
154750K .......... .......... .......... .......... .......... 59% 9.98M 12s
154800K .......... .......... .......... .......... .......... 59% 9.47M 12s
154850K .......... .......... .......... .......... .......... 59% 11.3M 12s
154900K .......... .......... .......... .......... .......... 59% 10.3M 12s
154950K .......... .......... .......... .......... .......... 59% 10.0M 12s
155000K .......... .......... .......... .......... .......... 59% 12.3M 12s
155050K .......... .......... .......... .......... .......... 59% 17.9M 12s
155100K .......... .......... .......... .......... .......... 59% 10.7M 12s
155150K .......... .......... .......... .......... .......... 59% 12.4M 12s
155200K .......... .......... .......... .......... .......... 59% 11.8M 12s
155250K .......... .......... .......... .......... .......... 59% 10.3M 12s
155300K .......... .......... .......... .......... .......... 59% 9.22M 12s
155350K .......... .......... .......... .......... .......... 59% 10.9M 12s
155400K .......... .......... .......... .......... .......... 59% 8.96M 12s
155450K .......... .......... .......... .......... .......... 59% 6.11M 12s
155500K .......... .......... .......... .......... .......... 59% 7.36M 12s
155550K .......... .......... .......... .......... .......... 59% 18.3M 12s
155600K .......... .......... .......... .......... .......... 59% 15.3M 12s
155650K .......... .......... .......... .......... .......... 59% 15.4M 12s
155700K .......... .......... .......... .......... .......... 59% 14.8M 12s
155750K .......... .......... .......... .......... .......... 59% 16.2M 12s
155800K .......... .......... .......... .......... .......... 59% 15.7M 12s
155850K .......... .......... .......... .......... .......... 59% 17.0M 12s
155900K .......... .......... .......... .......... .......... 59% 11.6M 12s
155950K .......... .......... .......... .......... .......... 59% 12.0M 12s
156000K .......... .......... .......... .......... .......... 59% 15.5M 12s
156050K .......... .......... .......... .......... .......... 59% 21.9M 12s
156100K .......... .......... .......... .......... .......... 59% 11.5M 12s
156150K .......... .......... .......... .......... .......... 59% 15.4M 12s
156200K .......... .......... .......... .......... .......... 59% 8.48M 12s
156250K .......... .......... .......... .......... .......... 59% 30.7M 12s
156300K .......... .......... .......... .......... .......... 59% 11.3M 12s
156350K .......... .......... .......... .......... .......... 59% 11.4M 12s
156400K .......... .......... .......... .......... .......... 59% 11.9M 12s
156450K .......... .......... .......... .......... .......... 59% 12.2M 12s
156500K .......... .......... .......... .......... .......... 59% 10.2M 12s
156550K .......... .......... .......... .......... .......... 59% 9.39M 12s
156600K .......... .......... .......... .......... .......... 59% 4.05M 12s
156650K .......... .......... .......... .......... .......... 59% 3.80M 12s
156700K .......... .......... .......... .......... .......... 59% 3.32M 12s
156750K .......... .......... .......... .......... .......... 59% 1.66M 12s
156800K .......... .......... .......... .......... .......... 59%  644K 12s
156850K .......... .......... .......... .......... .......... 59% 1.44M 12s
156900K .......... .......... .......... .......... .......... 59% 3.04M 12s
156950K .......... .......... .......... .......... .......... 59% 2.83M 12s
157000K .......... .......... .......... .......... .......... 59% 3.14M 12s
157050K .......... .......... .......... .......... .......... 59% 7.47M 12s
157100K .......... .......... .......... .......... .......... 59% 15.5M 12s
157150K .......... .......... .......... .......... .......... 59%  103M 12s
157200K .......... .......... .......... .......... .......... 59% 22.5M 12s
157250K .......... .......... .......... .......... .......... 59% 21.5M 12s
157300K .......... .......... .......... .......... .......... 60% 13.1M 12s
157350K .......... .......... .......... .......... .......... 60% 18.0M 12s
157400K .......... .......... .......... .......... .......... 60% 18.6M 12s
157450K .......... .......... .......... .......... .......... 60% 16.8M 12s
157500K .......... .......... .......... .......... .......... 60% 20.7M 12s
157550K .......... .......... .......... .......... .......... 60% 16.2M 12s
157600K .......... .......... .......... .......... .......... 60% 11.6M 12s
157650K .......... .......... .......... .......... .......... 60% 12.8M 12s
157700K .......... .......... .......... .......... .......... 60% 11.8M 12s
157750K .......... .......... .......... .......... .......... 60% 12.8M 12s
157800K .......... .......... .......... .......... .......... 60% 13.5M 12s
157850K .......... .......... .......... .......... .......... 60% 13.7M 12s
157900K .......... .......... .......... .......... .......... 60% 16.2M 12s
157950K .......... .......... .......... .......... .......... 60% 13.8M 12s
158000K .......... .......... .......... .......... .......... 60% 13.3M 12s
158050K .......... .......... .......... .......... .......... 60% 14.9M 12s
158100K .......... .......... .......... .......... .......... 60% 14.7M 12s
158150K .......... .......... .......... .......... .......... 60% 17.1M 12s
158200K .......... .......... .......... .......... .......... 60% 13.8M 12s
158250K .......... .......... .......... .......... .......... 60% 24.7M 12s
158300K .......... .......... .......... .......... .......... 60% 17.1M 12s
158350K .......... .......... .......... .......... .......... 60% 16.3M 12s
158400K .......... .......... .......... .......... .......... 60% 17.6M 12s
158450K .......... .......... .......... .......... .......... 60% 17.5M 12s
158500K .......... .......... .......... .......... .......... 60% 10.7M 12s
158550K .......... .......... .......... .......... .......... 60% 19.3M 12s
158600K .......... .......... .......... .......... .......... 60% 10.7M 12s
158650K .......... .......... .......... .......... .......... 60% 24.0M 12s
158700K .......... .......... .......... .......... .......... 60% 19.0M 12s
158750K .......... .......... .......... .......... .......... 60% 15.3M 12s
158800K .......... .......... .......... .......... .......... 60% 23.9M 12s
158850K .......... .......... .......... .......... .......... 60% 19.4M 12s
158900K .......... .......... .......... .......... .......... 60% 19.4M 12s
158950K .......... .......... .......... .......... .......... 60% 13.8M 12s
159000K .......... .......... .......... .......... .......... 60% 19.4M 12s
159050K .......... .......... .......... .......... .......... 60% 19.0M 12s
159100K .......... .......... .......... .......... .......... 60% 22.2M 12s
159150K .......... .......... .......... .......... .......... 60% 18.1M 12s
159200K .......... .......... .......... .......... .......... 60% 13.9M 12s
159250K .......... .......... .......... .......... .......... 60% 14.1M 12s
159300K .......... .......... .......... .......... .......... 60% 15.4M 12s
159350K .......... .......... .......... .......... .......... 60% 14.2M 12s
159400K .......... .......... .......... .......... .......... 60% 11.2M 12s
159450K .......... .......... .......... .......... .......... 60% 8.83M 12s
159500K .......... .......... .......... .......... .......... 60% 8.53M 12s
159550K .......... .......... .......... .......... .......... 60% 7.00M 12s
159600K .......... .......... .......... .......... .......... 60% 5.95M 12s
159650K .......... .......... .......... .......... .......... 60% 10.2M 12s
159700K .......... .......... .......... .......... .......... 60% 19.5M 12s
159750K .......... .......... .......... .......... .......... 60% 27.2M 12s
159800K .......... .......... .......... .......... .......... 60% 16.2M 12s
159850K .......... .......... .......... .......... .......... 60% 42.6M 12s
159900K .......... .......... .......... .......... .......... 61% 25.7M 12s
159950K .......... .......... .......... .......... .......... 61% 21.8M 12s
160000K .......... .......... .......... .......... .......... 61% 16.8M 12s
160050K .......... .......... .......... .......... .......... 61% 29.1M 12s
160100K .......... .......... .......... .......... .......... 61% 13.8M 12s
160150K .......... .......... .......... .......... .......... 61% 19.0M 12s
160200K .......... .......... .......... .......... .......... 61% 10.3M 12s
160250K .......... .......... .......... .......... .......... 61% 16.3M 12s
160300K .......... .......... .......... .......... .......... 61% 18.0M 12s
160350K .......... .......... .......... .......... .......... 61% 17.0M 12s
160400K .......... .......... .......... .......... .......... 61% 15.4M 12s
160450K .......... .......... .......... .......... .......... 61% 20.4M 12s
160500K .......... .......... .......... .......... .......... 61% 27.2M 11s
160550K .......... .......... .......... .......... .......... 61% 13.3M 11s
160600K .......... .......... .......... .......... .......... 61% 13.8M 11s
160650K .......... .......... .......... .......... .......... 61% 9.56M 11s
160700K .......... .......... .......... .......... .......... 61% 24.4M 11s
160750K .......... .......... .......... .......... .......... 61% 14.3M 11s
160800K .......... .......... .......... .......... .......... 61% 10.5M 11s
160850K .......... .......... .......... .......... .......... 61% 8.10M 11s
160900K .......... .......... .......... .......... .......... 61% 5.93M 11s
160950K .......... .......... .......... .......... .......... 61% 9.35M 11s
161000K .......... .......... .......... .......... .......... 61% 9.36M 11s
161050K .......... .......... .......... .......... .......... 61% 18.6M 11s
161100K .......... .......... .......... .......... .......... 61% 16.5M 11s
161150K .......... .......... .......... .......... .......... 61% 24.0M 11s
161200K .......... .......... .......... .......... .......... 61% 12.9M 11s
161250K .......... .......... .......... .......... .......... 61% 18.2M 11s
161300K .......... .......... .......... .......... .......... 61% 17.4M 11s
161350K .......... .......... .......... .......... .......... 61% 14.2M 11s
161400K .......... .......... .......... .......... .......... 61% 19.0M 11s
161450K .......... .......... .......... .......... .......... 61% 14.5M 11s
161500K .......... .......... .......... .......... .......... 61% 10.7M 11s
161550K .......... .......... .......... .......... .......... 61% 11.0M 11s
161600K .......... .......... .......... .......... .......... 61% 8.65M 11s
161650K .......... .......... .......... .......... .......... 61%  916K 11s
161700K .......... .......... .......... .......... .......... 61% 6.56M 11s
161750K .......... .......... .......... .......... .......... 61% 22.4M 11s
161800K .......... .......... .......... .......... .......... 61% 15.6M 11s
161850K .......... .......... .......... .......... .......... 61% 18.0M 11s
161900K .......... .......... .......... .......... .......... 61% 20.2M 11s
161950K .......... .......... .......... .......... .......... 61% 10.4M 11s
162000K .......... .......... .......... .......... .......... 61% 13.2M 11s
162050K .......... .......... .......... .......... .......... 61% 13.9M 11s
162100K .......... .......... .......... .......... .......... 61% 5.17M 11s
162150K .......... .......... .......... .......... .......... 61% 7.10M 11s
162200K .......... .......... .......... .......... .......... 61% 13.2M 11s
162250K .......... .......... .......... .......... .......... 61% 21.1M 11s
162300K .......... .......... .......... .......... .......... 61% 16.2M 11s
162350K .......... .......... .......... .......... .......... 61% 13.3M 11s
162400K .......... .......... .......... .......... .......... 61% 15.8M 11s
162450K .......... .......... .......... .......... .......... 61% 12.4M 11s
162500K .......... .......... .......... .......... .......... 61% 16.9M 11s
162550K .......... .......... .......... .......... .......... 62% 19.7M 11s
162600K .......... .......... .......... .......... .......... 62% 19.9M 11s
162650K .......... .......... .......... .......... .......... 62% 21.2M 11s
162700K .......... .......... .......... .......... .......... 62% 17.3M 11s
162750K .......... .......... .......... .......... .......... 62% 39.3M 11s
162800K .......... .......... .......... .......... .......... 62% 18.3M 11s
162850K .......... .......... .......... .......... .......... 62% 13.1M 11s
162900K .......... .......... .......... .......... .......... 62% 18.6M 11s
162950K .......... .......... .......... .......... .......... 62% 17.2M 11s
163000K .......... .......... .......... .......... .......... 62% 22.0M 11s
163050K .......... .......... .......... .......... .......... 62% 16.6M 11s
163100K .......... .......... .......... .......... .......... 62% 13.5M 11s
163150K .......... .......... .......... .......... .......... 62% 20.0M 11s
163200K .......... .......... .......... .......... .......... 62% 17.4M 11s
163250K .......... .......... .......... .......... .......... 62% 11.0M 11s
163300K .......... .......... .......... .......... .......... 62% 17.2M 11s
163350K .......... .......... .......... .......... .......... 62% 13.3M 11s
163400K .......... .......... .......... .......... .......... 62% 15.3M 11s
163450K .......... .......... .......... .......... .......... 62% 9.11M 11s
163500K .......... .......... .......... .......... .......... 62% 13.8M 11s
163550K .......... .......... .......... .......... .......... 62% 11.6M 11s
163600K .......... .......... .......... .......... .......... 62% 11.6M 11s
163650K .......... .......... .......... .......... .......... 62% 22.7M 11s
163700K .......... .......... .......... .......... .......... 62% 12.9M 11s
163750K .......... .......... .......... .......... .......... 62% 22.0M 11s
163800K .......... .......... .......... .......... .......... 62% 11.4M 11s
163850K .......... .......... .......... .......... .......... 62% 10.5M 11s
163900K .......... .......... .......... .......... .......... 62% 15.8M 11s
163950K .......... .......... .......... .......... .......... 62% 10.4M 11s
164000K .......... .......... .......... .......... .......... 62% 14.1M 11s
164050K .......... .......... .......... .......... .......... 62% 19.8M 11s
164100K .......... .......... .......... .......... .......... 62% 11.8M 11s
164150K .......... .......... .......... .......... .......... 62% 14.3M 11s
164200K .......... .......... .......... .......... .......... 62% 26.7M 11s
164250K .......... .......... .......... .......... .......... 62% 43.3M 11s
164300K .......... .......... .......... .......... .......... 62% 27.2M 11s
164350K .......... .......... .......... .......... .......... 62% 31.8M 11s
164400K .......... .......... .......... .......... .......... 62% 32.2M 11s
164450K .......... .......... .......... .......... .......... 62% 22.8M 11s
164500K .......... .......... .......... .......... .......... 62% 44.9M 11s
164550K .......... .......... .......... .......... .......... 62% 18.4M 11s
164600K .......... .......... .......... .......... .......... 62% 36.5M 11s
164650K .......... .......... .......... .......... .......... 62% 24.2M 11s
164700K .......... .......... .......... .......... .......... 62% 17.2M 11s
164750K .......... .......... .......... .......... .......... 62% 27.3M 11s
164800K .......... .......... .......... .......... .......... 62% 21.4M 11s
164850K .......... .......... .......... .......... .......... 62% 20.3M 11s
164900K .......... .......... .......... .......... .......... 62% 20.5M 11s
164950K .......... .......... .......... .......... .......... 62% 19.0M 11s
165000K .......... .......... .......... .......... .......... 62% 16.7M 11s
165050K .......... .......... .......... .......... .......... 62% 14.7M 11s
165100K .......... .......... .......... .......... .......... 62% 14.0M 11s
165150K .......... .......... .......... .......... .......... 63% 18.7M 11s
165200K .......... .......... .......... .......... .......... 63% 11.3M 11s
165250K .......... .......... .......... .......... .......... 63% 19.1M 11s
165300K .......... .......... .......... .......... .......... 63% 23.8M 11s
165350K .......... .......... .......... .......... .......... 63% 17.7M 11s
165400K .......... .......... .......... .......... .......... 63% 21.0M 11s
165450K .......... .......... .......... .......... .......... 63% 15.5M 11s
165500K .......... .......... .......... .......... .......... 63% 21.1M 11s
165550K .......... .......... .......... .......... .......... 63% 20.3M 11s
165600K .......... .......... .......... .......... .......... 63% 18.6M 11s
165650K .......... .......... .......... .......... .......... 63% 11.5M 11s
165700K .......... .......... .......... .......... .......... 63% 14.8M 11s
165750K .......... .......... .......... .......... .......... 63% 15.6M 11s
165800K .......... .......... .......... .......... .......... 63% 17.5M 11s
165850K .......... .......... .......... .......... .......... 63% 12.3M 11s
165900K .......... .......... .......... .......... .......... 63% 13.9M 11s
165950K .......... .......... .......... .......... .......... 63% 8.79M 11s
166000K .......... .......... .......... .......... .......... 63% 16.8M 11s
166050K .......... .......... .......... .......... .......... 63% 20.3M 11s
166100K .......... .......... .......... .......... .......... 63% 23.4M 11s
166150K .......... .......... .......... .......... .......... 63% 17.0M 11s
166200K .......... .......... .......... .......... .......... 63% 10.4M 11s
166250K .......... .......... .......... .......... .......... 63% 15.0M 11s
166300K .......... .......... .......... .......... .......... 63% 18.8M 11s
166350K .......... .......... .......... .......... .......... 63% 13.9M 11s
166400K .......... .......... .......... .......... .......... 63% 15.7M 11s
166450K .......... .......... .......... .......... .......... 63% 10.2M 11s
166500K .......... .......... .......... .......... .......... 63% 11.3M 11s
166550K .......... .......... .......... .......... .......... 63% 14.7M 11s
166600K .......... .......... .......... .......... .......... 63% 16.7M 11s
166650K .......... .......... .......... .......... .......... 63% 22.1M 11s
166700K .......... .......... .......... .......... .......... 63% 17.6M 11s
166750K .......... .......... .......... .......... .......... 63% 18.9M 11s
166800K .......... .......... .......... .......... .......... 63% 23.0M 11s
166850K .......... .......... .......... .......... .......... 63% 18.3M 11s
166900K .......... .......... .......... .......... .......... 63% 17.6M 11s
166950K .......... .......... .......... .......... .......... 63% 26.1M 11s
167000K .......... .......... .......... .......... .......... 63% 22.3M 11s
167050K .......... .......... .......... .......... .......... 63% 21.1M 11s
167100K .......... .......... .......... .......... .......... 63% 19.9M 11s
167150K .......... .......... .......... .......... .......... 63% 14.1M 11s
167200K .......... .......... .......... .......... .......... 63% 29.2M 11s
167250K .......... .......... .......... .......... .......... 63% 20.8M 11s
167300K .......... .......... .......... .......... .......... 63% 21.6M 11s
167350K .......... .......... .......... .......... .......... 63% 17.6M 11s
167400K .......... .......... .......... .......... .......... 63% 20.4M 11s
167450K .......... .......... .......... .......... .......... 63% 19.9M 11s
167500K .......... .......... .......... .......... .......... 63% 22.5M 11s
167550K .......... .......... .......... .......... .......... 63% 25.7M 11s
167600K .......... .......... .......... .......... .......... 63% 19.6M 11s
167650K .......... .......... .......... .......... .......... 63% 16.0M 11s
167700K .......... .......... .......... .......... .......... 63% 15.6M 11s
167750K .......... .......... .......... .......... .......... 63% 22.2M 11s
167800K .......... .......... .......... .......... .......... 64% 21.4M 10s
167850K .......... .......... .......... .......... .......... 64% 11.5M 10s
167900K .......... .......... .......... .......... .......... 64% 14.7M 10s
167950K .......... .......... .......... .......... .......... 64% 8.86M 10s
168000K .......... .......... .......... .......... .......... 64% 12.3M 10s
168050K .......... .......... .......... .......... .......... 64% 18.8M 10s
168100K .......... .......... .......... .......... .......... 64% 18.6M 10s
168150K .......... .......... .......... .......... .......... 64% 19.7M 10s
168200K .......... .......... .......... .......... .......... 64% 13.2M 10s
168250K .......... .......... .......... .......... .......... 64% 19.5M 10s
168300K .......... .......... .......... .......... .......... 64% 21.1M 10s
168350K .......... .......... .......... .......... .......... 64% 18.7M 10s
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169000K .......... .......... .......... .......... .......... 64% 13.8M 10s
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169100K .......... .......... .......... .......... .......... 64% 17.3M 10s
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169250K .......... .......... .......... .......... .......... 64% 12.7M 10s
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170000K .......... .......... .......... .......... .......... 64% 33.7M 10s
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172150K .......... .......... .......... .......... .......... 65% 17.2M 10s
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181500K .......... .......... .......... .......... .......... 69% 14.2M 9s
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181800K .......... .......... .......... .......... .......... 69% 23.4M 9s
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182150K .......... .......... .......... .......... .......... 69% 22.0M 9s
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182250K .......... .......... .......... .......... .......... 69% 8.51M 9s
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182450K .......... .......... .......... .......... .......... 69% 35.7M 9s
182500K .......... .......... .......... .......... .......... 69% 39.3M 9s
182550K .......... .......... .......... .......... .......... 69% 40.9M 9s
182600K .......... .......... .......... .......... .......... 69% 24.3M 9s
182650K .......... .......... .......... .......... .......... 69% 20.3M 9s
182700K .......... .......... .......... .......... .......... 69% 28.0M 9s
182750K .......... .......... .......... .......... .......... 69% 26.8M 9s
182800K .......... .......... .......... .......... .......... 69% 19.1M 9s
182850K .......... .......... .......... .......... .......... 69% 39.6M 8s
182900K .......... .......... .......... .......... .......... 69% 29.2M 8s
182950K .......... .......... .......... .......... .......... 69% 23.3M 8s
183000K .......... .......... .......... .......... .......... 69% 20.9M 8s
183050K .......... .......... .......... .......... .......... 69% 15.3M 8s
183100K .......... .......... .......... .......... .......... 69% 15.4M 8s
183150K .......... .......... .......... .......... .......... 69% 19.1M 8s
183200K .......... .......... .......... .......... .......... 69% 21.5M 8s
183250K .......... .......... .......... .......... .......... 69% 18.5M 8s
183300K .......... .......... .......... .......... .......... 69% 16.1M 8s
183350K .......... .......... .......... .......... .......... 69% 9.77M 8s
183400K .......... .......... .......... .......... .......... 69% 18.4M 8s
183450K .......... .......... .......... .......... .......... 69% 15.8M 8s
183500K .......... .......... .......... .......... .......... 70% 11.0M 8s
183550K .......... .......... .......... .......... .......... 70% 31.5M 8s
183600K .......... .......... .......... .......... .......... 70% 22.9M 8s
183650K .......... .......... .......... .......... .......... 70% 22.8M 8s
183700K .......... .......... .......... .......... .......... 70% 18.3M 8s
183750K .......... .......... .......... .......... .......... 70% 16.0M 8s
183800K .......... .......... .......... .......... .......... 70% 22.2M 8s
183850K .......... .......... .......... .......... .......... 70% 16.4M 8s
183900K .......... .......... .......... .......... .......... 70% 24.4M 8s
183950K .......... .......... .......... .......... .......... 70% 19.3M 8s
184000K .......... .......... .......... .......... .......... 70% 22.0M 8s
184050K .......... .......... .......... .......... .......... 70% 31.8M 8s
184100K .......... .......... .......... .......... .......... 70% 17.7M 8s
184150K .......... .......... .......... .......... .......... 70% 20.8M 8s
184200K .......... .......... .......... .......... .......... 70% 19.3M 8s
184250K .......... .......... .......... .......... .......... 70% 15.1M 8s
184300K .......... .......... .......... .......... .......... 70% 49.6M 8s
184350K .......... .......... .......... .......... .......... 70% 23.0M 8s
184400K .......... .......... .......... .......... .......... 70% 24.1M 8s
184450K .......... .......... .......... .......... .......... 70% 21.8M 8s
184500K .......... .......... .......... .......... .......... 70% 20.8M 8s
184550K .......... .......... .......... .......... .......... 70% 24.0M 8s
184600K .......... .......... .......... .......... .......... 70% 24.2M 8s
184650K .......... .......... .......... .......... .......... 70% 17.6M 8s
184700K .......... .......... .......... .......... .......... 70% 16.2M 8s
184750K .......... .......... .......... .......... .......... 70% 44.3M 8s
184800K .......... .......... .......... .......... .......... 70% 26.0M 8s
184850K .......... .......... .......... .......... .......... 70% 21.2M 8s
184900K .......... .......... .......... .......... .......... 70% 14.8M 8s
184950K .......... .......... .......... .......... .......... 70% 17.3M 8s
185000K .......... .......... .......... .......... .......... 70% 18.0M 8s
185050K .......... .......... .......... .......... .......... 70% 26.8M 8s
185100K .......... .......... .......... .......... .......... 70% 15.7M 8s
185150K .......... .......... .......... .......... .......... 70% 12.5M 8s
185200K .......... .......... .......... .......... .......... 70% 12.6M 8s
185250K .......... .......... .......... .......... .......... 70% 16.8M 8s
185300K .......... .......... .......... .......... .......... 70% 16.7M 8s
185350K .......... .......... .......... .......... .......... 70% 13.9M 8s
185400K .......... .......... .......... .......... .......... 70% 19.5M 8s
185450K .......... .......... .......... .......... .......... 70% 15.7M 8s
185500K .......... .......... .......... .......... .......... 70% 17.5M 8s
185550K .......... .......... .......... .......... .......... 70% 20.0M 8s
185600K .......... .......... .......... .......... .......... 70% 17.1M 8s
185650K .......... .......... .......... .......... .......... 70% 30.9M 8s
185700K .......... .......... .......... .......... .......... 70% 13.7M 8s
185750K .......... .......... .......... .......... .......... 70% 14.0M 8s
185800K .......... .......... .......... .......... .......... 70% 13.9M 8s
185850K .......... .......... .......... .......... .......... 70% 12.3M 8s
185900K .......... .......... .......... .......... .......... 70% 12.5M 8s
185950K .......... .......... .......... .......... .......... 70% 11.8M 8s
186000K .......... .......... .......... .......... .......... 70% 29.9M 8s
186050K .......... .......... .......... .......... .......... 70% 23.9M 8s
186100K .......... .......... .......... .......... .......... 70% 19.7M 8s
186150K .......... .......... .......... .......... .......... 71% 24.0M 8s
186200K .......... .......... .......... .......... .......... 71% 18.1M 8s
186250K .......... .......... .......... .......... .......... 71% 29.7M 8s
186300K .......... .......... .......... .......... .......... 71% 24.6M 8s
186350K .......... .......... .......... .......... .......... 71% 21.6M 8s
186400K .......... .......... .......... .......... .......... 71% 22.6M 8s
186450K .......... .......... .......... .......... .......... 71% 14.8M 8s
186500K .......... .......... .......... .......... .......... 71% 40.1M 8s
186550K .......... .......... .......... .......... .......... 71% 24.8M 8s
186600K .......... .......... .......... .......... .......... 71% 21.1M 8s
186650K .......... .......... .......... .......... .......... 71% 24.3M 8s
186700K .......... .......... .......... .......... .......... 71% 19.7M 8s
186750K .......... .......... .......... .......... .......... 71% 22.0M 8s
186800K .......... .......... .......... .......... .......... 71% 25.4M 8s
186850K .......... .......... .......... .......... .......... 71% 21.3M 8s
186900K .......... .......... .......... .......... .......... 71% 23.2M 8s
186950K .......... .......... .......... .......... .......... 71% 20.9M 8s
187000K .......... .......... .......... .......... .......... 71% 19.5M 8s
187050K .......... .......... .......... .......... .......... 71% 27.3M 8s
187100K .......... .......... .......... .......... .......... 71% 18.7M 8s
187150K .......... .......... .......... .......... .......... 71% 24.1M 8s
187200K .......... .......... .......... .......... .......... 71% 16.9M 8s
187250K .......... .......... .......... .......... .......... 71% 17.2M 8s
187300K .......... .......... .......... .......... .......... 71% 17.3M 8s
187350K .......... .......... .......... .......... .......... 71% 15.4M 8s
187400K .......... .......... .......... .......... .......... 71% 21.4M 8s
187450K .......... .......... .......... .......... .......... 71% 16.4M 8s
187500K .......... .......... .......... .......... .......... 71% 20.2M 8s
187550K .......... .......... .......... .......... .......... 71% 14.3M 8s
187600K .......... .......... .......... .......... .......... 71% 13.6M 8s
187650K .......... .......... .......... .......... .......... 71% 18.5M 8s
187700K .......... .......... .......... .......... .......... 71% 6.85M 8s
187750K .......... .......... .......... .......... .......... 71% 8.53M 8s
187800K .......... .......... .......... .......... .......... 71% 14.0M 8s
187850K .......... .......... .......... .......... .......... 71% 12.7M 8s
187900K .......... .......... .......... .......... .......... 71% 16.0M 8s
187950K .......... .......... .......... .......... .......... 71% 11.7M 8s
188000K .......... .......... .......... .......... .......... 71% 20.2M 8s
188050K .......... .......... .......... .......... .......... 71% 17.3M 8s
188100K .......... .......... .......... .......... .......... 71% 11.2M 8s
188150K .......... .......... .......... .......... .......... 71% 12.2M 8s
188200K .......... .......... .......... .......... .......... 71% 7.78M 8s
188250K .......... .......... .......... .......... .......... 71% 8.20M 8s
188300K .......... .......... .......... .......... .......... 71% 14.1M 8s
188350K .......... .......... .......... .......... .......... 71% 17.5M 8s
188400K .......... .......... .......... .......... .......... 71% 12.0M 8s
188450K .......... .......... .......... .......... .......... 71% 15.2M 8s
188500K .......... .......... .......... .......... .......... 71% 15.4M 8s
188550K .......... .......... .......... .......... .......... 71% 21.9M 8s
188600K .......... .......... .......... .......... .......... 71% 13.1M 8s
188650K .......... .......... .......... .......... .......... 71% 21.6M 8s
188700K .......... .......... .......... .......... .......... 71% 10.1M 8s
188750K .......... .......... .......... .......... .......... 72% 20.3M 8s
188800K .......... .......... .......... .......... .......... 72% 17.3M 8s
188850K .......... .......... .......... .......... .......... 72% 11.8M 8s
188900K .......... .......... .......... .......... .......... 72% 13.1M 8s
188950K .......... .......... .......... .......... .......... 72% 13.6M 8s
189000K .......... .......... .......... .......... .......... 72% 15.4M 8s
189050K .......... .......... .......... .......... .......... 72% 28.7M 8s
189100K .......... .......... .......... .......... .......... 72% 11.4M 8s
189150K .......... .......... .......... .......... .......... 72% 12.3M 8s
189200K .......... .......... .......... .......... .......... 72% 9.45M 8s
189250K .......... .......... .......... .......... .......... 72% 12.1M 8s
189300K .......... .......... .......... .......... .......... 72% 17.3M 8s
189350K .......... .......... .......... .......... .......... 72% 12.7M 8s
189400K .......... .......... .......... .......... .......... 72% 15.3M 8s
189450K .......... .......... .......... .......... .......... 72% 13.9M 8s
189500K .......... .......... .......... .......... .......... 72% 13.7M 8s
189550K .......... .......... .......... .......... .......... 72% 11.7M 8s
189600K .......... .......... .......... .......... .......... 72% 10.5M 8s
189650K .......... .......... .......... .......... .......... 72% 11.1M 8s
189700K .......... .......... .......... .......... .......... 72% 8.09M 8s
189750K .......... .......... .......... .......... .......... 72% 2.11M 8s
189800K .......... .......... .......... .......... .......... 72% 1.71M 8s
189850K .......... .......... .......... .......... .......... 72% 8.61M 8s
189900K .......... .......... .......... .......... .......... 72% 10.5M 8s
189950K .......... .......... .......... .......... .......... 72% 11.4M 8s
190000K .......... .......... .......... .......... .......... 72% 13.1M 8s
190050K .......... .......... .......... .......... .......... 72% 21.2M 8s
190100K .......... .......... .......... .......... .......... 72% 23.2M 8s
190150K .......... .......... .......... .......... .......... 72% 17.3M 8s
190200K .......... .......... .......... .......... .......... 72% 18.0M 8s
190250K .......... .......... .......... .......... .......... 72% 17.6M 8s
190300K .......... .......... .......... .......... .......... 72% 17.3M 8s
190350K .......... .......... .......... .......... .......... 72% 20.3M 8s
190400K .......... .......... .......... .......... .......... 72% 19.9M 8s
190450K .......... .......... .......... .......... .......... 72% 12.9M 8s
190500K .......... .......... .......... .......... .......... 72% 16.2M 8s
190550K .......... .......... .......... .......... .......... 72% 19.1M 8s
190600K .......... .......... .......... .......... .......... 72% 9.91M 8s
190650K .......... .......... .......... .......... .......... 72% 18.9M 8s
190700K .......... .......... .......... .......... .......... 72% 11.0M 8s
190750K .......... .......... .......... .......... .......... 72% 15.3M 8s
190800K .......... .......... .......... .......... .......... 72% 16.0M 8s
190850K .......... .......... .......... .......... .......... 72% 15.8M 8s
190900K .......... .......... .......... .......... .......... 72% 17.6M 8s
190950K .......... .......... .......... .......... .......... 72% 13.5M 8s
191000K .......... .......... .......... .......... .......... 72% 20.8M 8s
191050K .......... .......... .......... .......... .......... 72% 16.9M 7s
191100K .......... .......... .......... .......... .......... 72% 12.3M 7s
191150K .......... .......... .......... .......... .......... 72% 7.71M 7s
191200K .......... .......... .......... .......... .......... 72% 6.33M 7s
191250K .......... .......... .......... .......... .......... 72% 5.82M 7s
191300K .......... .......... .......... .......... .......... 72% 7.21M 7s
191350K .......... .......... .......... .......... .......... 72% 5.80M 7s
191400K .......... .......... .......... .......... .......... 73% 8.70M 7s
191450K .......... .......... .......... .......... .......... 73% 7.03M 7s
191500K .......... .......... .......... .......... .......... 73% 11.0M 7s
191550K .......... .......... .......... .......... .......... 73% 7.06M 7s
191600K .......... .......... .......... .......... .......... 73% 4.15M 7s
191650K .......... .......... .......... .......... .......... 73% 4.32M 7s
191700K .......... .......... .......... .......... .......... 73% 3.13M 7s
191750K .......... .......... .......... .......... .......... 73% 3.85M 7s
191800K .......... .......... .......... .......... .......... 73% 3.53M 7s
191850K .......... .......... .......... .......... .......... 73% 5.28M 7s
191900K .......... .......... .......... .......... .......... 73% 9.26M 7s
191950K .......... .......... .......... .......... .......... 73% 7.35M 7s
192000K .......... .......... .......... .......... .......... 73% 8.93M 7s
192050K .......... .......... .......... .......... .......... 73% 9.89M 7s
192100K .......... .......... .......... .......... .......... 73% 8.90M 7s
192150K .......... .......... .......... .......... .......... 73% 11.4M 7s
192200K .......... .......... .......... .......... .......... 73% 10.6M 7s
192250K .......... .......... .......... .......... .......... 73% 11.8M 7s
192300K .......... .......... .......... .......... .......... 73% 11.8M 7s
192350K .......... .......... .......... .......... .......... 73% 11.5M 7s
192400K .......... .......... .......... .......... .......... 73% 8.85M 7s
192450K .......... .......... .......... .......... .......... 73% 6.57M 7s
192500K .......... .......... .......... .......... .......... 73% 8.86M 7s
192550K .......... .......... .......... .......... .......... 73% 8.66M 7s
192600K .......... .......... .......... .......... .......... 73% 12.4M 7s
192650K .......... .......... .......... .......... .......... 73% 17.0M 7s
192700K .......... .......... .......... .......... .......... 73% 12.3M 7s
192750K .......... .......... .......... .......... .......... 73% 15.7M 7s
192800K .......... .......... .......... .......... .......... 73% 16.5M 7s
192850K .......... .......... .......... .......... .......... 73% 12.6M 7s
192900K .......... .......... .......... .......... .......... 73% 20.5M 7s
192950K .......... .......... .......... .......... .......... 73% 14.9M 7s
193000K .......... .......... .......... .......... .......... 73% 20.3M 7s
193050K .......... .......... .......... .......... .......... 73% 22.7M 7s
193100K .......... .......... .......... .......... .......... 73% 15.8M 7s
193150K .......... .......... .......... .......... .......... 73% 24.5M 7s
193200K .......... .......... .......... .......... .......... 73% 17.7M 7s
193250K .......... .......... .......... .......... .......... 73% 14.5M 7s
193300K .......... .......... .......... .......... .......... 73% 26.1M 7s
193350K .......... .......... .......... .......... .......... 73% 18.2M 7s
193400K .......... .......... .......... .......... .......... 73% 40.8M 7s
193450K .......... .......... .......... .......... .......... 73% 20.1M 7s
193500K .......... .......... .......... .......... .......... 73% 16.5M 7s
193550K .......... .......... .......... .......... .......... 73% 12.9M 7s
193600K .......... .......... .......... .......... .......... 73% 11.6M 7s
193650K .......... .......... .......... .......... .......... 73% 13.9M 7s
193700K .......... .......... .......... .......... .......... 73% 12.6M 7s
193750K .......... .......... .......... .......... .......... 73% 13.3M 7s
193800K .......... .......... .......... .......... .......... 73% 11.6M 7s
193850K .......... .......... .......... .......... .......... 73% 11.2M 7s
193900K .......... .......... .......... .......... .......... 73% 18.3M 7s
193950K .......... .......... .......... .......... .......... 73% 14.6M 7s
194000K .......... .......... .......... .......... .......... 74% 18.1M 7s
194050K .......... .......... .......... .......... .......... 74% 14.0M 7s
194100K .......... .......... .......... .......... .......... 74% 10.3M 7s
194150K .......... .......... .......... .......... .......... 74% 15.0M 7s
194200K .......... .......... .......... .......... .......... 74% 10.5M 7s
194250K .......... .......... .......... .......... .......... 74% 16.8M 7s
194300K .......... .......... .......... .......... .......... 74% 16.7M 7s
194350K .......... .......... .......... .......... .......... 74% 8.39M 7s
194400K .......... .......... .......... .......... .......... 74% 6.71M 7s
194450K .......... .......... .......... .......... .......... 74% 12.5M 7s
194500K .......... .......... .......... .......... .......... 74% 13.1M 7s
194550K .......... .......... .......... .......... .......... 74% 8.52M 7s
194600K .......... .......... .......... .......... .......... 74% 7.73M 7s
194650K .......... .......... .......... .......... .......... 74% 7.57M 7s
194700K .......... .......... .......... .......... .......... 74% 10.2M 7s
194750K .......... .......... .......... .......... .......... 74% 11.1M 7s
194800K .......... .......... .......... .......... .......... 74% 10.4M 7s
194850K .......... .......... .......... .......... .......... 74% 12.5M 7s
194900K .......... .......... .......... .......... .......... 74% 16.5M 7s
194950K .......... .......... .......... .......... .......... 74% 20.3M 7s
195000K .......... .......... .......... .......... .......... 74% 21.8M 7s
195050K .......... .......... .......... .......... .......... 74% 21.6M 7s
195100K .......... .......... .......... .......... .......... 74% 16.9M 7s
195150K .......... .......... .......... .......... .......... 74% 24.7M 7s
195200K .......... .......... .......... .......... .......... 74% 16.7M 7s
195250K .......... .......... .......... .......... .......... 74% 19.4M 7s
195300K .......... .......... .......... .......... .......... 74% 19.9M 7s
195350K .......... .......... .......... .......... .......... 74% 12.4M 7s
195400K .......... .......... .......... .......... .......... 74% 19.5M 7s
195450K .......... .......... .......... .......... .......... 74% 22.5M 7s
195500K .......... .......... .......... .......... .......... 74% 22.1M 7s
195550K .......... .......... .......... .......... .......... 74% 12.6M 7s
195600K .......... .......... .......... .......... .......... 74% 15.4M 7s
195650K .......... .......... .......... .......... .......... 74% 17.6M 7s
195700K .......... .......... .......... .......... .......... 74% 14.4M 7s
195750K .......... .......... .......... .......... .......... 74% 18.7M 7s
195800K .......... .......... .......... .......... .......... 74% 16.4M 7s
195850K .......... .......... .......... .......... .......... 74% 12.8M 7s
195900K .......... .......... .......... .......... .......... 74% 10.6M 7s
195950K .......... .......... .......... .......... .......... 74% 11.9M 7s
196000K .......... .......... .......... .......... .......... 74% 15.2M 7s
196050K .......... .......... .......... .......... .......... 74% 13.3M 7s
196100K .......... .......... .......... .......... .......... 74% 8.40M 7s
196150K .......... .......... .......... .......... .......... 74% 9.69M 7s
196200K .......... .......... .......... .......... .......... 74% 12.6M 7s
196250K .......... .......... .......... .......... .......... 74% 15.3M 7s
196300K .......... .......... .......... .......... .......... 74% 16.7M 7s
196350K .......... .......... .......... .......... .......... 74% 8.82M 7s
196400K .......... .......... .......... .......... .......... 74% 24.4M 7s
196450K .......... .......... .......... .......... .......... 74% 17.2M 7s
196500K .......... .......... .......... .......... .......... 74% 32.1M 7s
196550K .......... .......... .......... .......... .......... 74% 18.2M 7s
196600K .......... .......... .......... .......... .......... 75% 16.8M 7s
196650K .......... .......... .......... .......... .......... 75% 12.6M 7s
196700K .......... .......... .......... .......... .......... 75% 8.37M 7s
196750K .......... .......... .......... .......... .......... 75% 17.5M 7s
196800K .......... .......... .......... .......... .......... 75% 15.9M 7s
196850K .......... .......... .......... .......... .......... 75% 17.6M 7s
196900K .......... .......... .......... .......... .......... 75% 24.1M 7s
196950K .......... .......... .......... .......... .......... 75% 20.4M 7s
197000K .......... .......... .......... .......... .......... 75% 19.2M 7s
197050K .......... .......... .......... .......... .......... 75% 18.7M 7s
197100K .......... .......... .......... .......... .......... 75% 13.8M 7s
197150K .......... .......... .......... .......... .......... 75% 26.4M 7s
197200K .......... .......... .......... .......... .......... 75% 13.5M 7s
197250K .......... .......... .......... .......... .......... 75% 21.7M 7s
197300K .......... .......... .......... .......... .......... 75% 16.7M 7s
197350K .......... .......... .......... .......... .......... 75% 37.2M 7s
197400K .......... .......... .......... .......... .......... 75% 31.5M 7s
197450K .......... .......... .......... .......... .......... 75% 24.8M 7s
197500K .......... .......... .......... .......... .......... 75% 28.2M 7s
197550K .......... .......... .......... .......... .......... 75% 32.2M 7s
197600K .......... .......... .......... .......... .......... 75% 20.5M 7s
197650K .......... .......... .......... .......... .......... 75% 17.0M 7s
197700K .......... .......... .......... .......... .......... 75% 20.4M 7s
197750K .......... .......... .......... .......... .......... 75% 25.5M 7s
197800K .......... .......... .......... .......... .......... 75% 15.4M 7s
197850K .......... .......... .......... .......... .......... 75% 12.4M 7s
197900K .......... .......... .......... .......... .......... 75% 25.8M 7s
197950K .......... .......... .......... .......... .......... 75% 67.8M 7s
198000K .......... .......... .......... .......... .......... 75% 38.4M 7s
198050K .......... .......... .......... .......... .......... 75% 33.6M 7s
198100K .......... .......... .......... .......... .......... 75% 23.3M 7s
198150K .......... .......... .......... .......... .......... 75% 16.0M 7s
198200K .......... .......... .......... .......... .......... 75% 29.2M 7s
198250K .......... .......... .......... .......... .......... 75% 18.2M 7s
198300K .......... .......... .......... .......... .......... 75% 29.3M 7s
198350K .......... .......... .......... .......... .......... 75% 19.7M 7s
198400K .......... .......... .......... .......... .......... 75% 31.1M 7s
198450K .......... .......... .......... .......... .......... 75% 17.2M 7s
198500K .......... .......... .......... .......... .......... 75% 15.3M 7s
198550K .......... .......... .......... .......... .......... 75% 23.9M 7s
198600K .......... .......... .......... .......... .......... 75% 17.2M 7s
198650K .......... .......... .......... .......... .......... 75% 17.7M 7s
198700K .......... .......... .......... .......... .......... 75% 21.0M 7s
198750K .......... .......... .......... .......... .......... 75% 19.6M 7s
198800K .......... .......... .......... .......... .......... 75% 17.1M 7s
198850K .......... .......... .......... .......... .......... 75% 11.7M 7s
198900K .......... .......... .......... .......... .......... 75% 15.1M 7s
198950K .......... .......... .......... .......... .......... 75% 14.2M 7s
199000K .......... .......... .......... .......... .......... 75% 17.5M 7s
199050K .......... .......... .......... .......... .......... 75% 19.4M 7s
199100K .......... .......... .......... .......... .......... 75% 20.2M 7s
199150K .......... .......... .......... .......... .......... 75% 13.4M 7s
199200K .......... .......... .......... .......... .......... 75% 22.7M 7s
199250K .......... .......... .......... .......... .......... 76% 16.8M 7s
199300K .......... .......... .......... .......... .......... 76% 19.0M 7s
199350K .......... .......... .......... .......... .......... 76% 12.6M 7s
199400K .......... .......... .......... .......... .......... 76% 20.1M 7s
199450K .......... .......... .......... .......... .......... 76% 18.2M 7s
199500K .......... .......... .......... .......... .......... 76% 26.6M 7s
199550K .......... .......... .......... .......... .......... 76% 29.0M 7s
199600K .......... .......... .......... .......... .......... 76% 21.7M 7s
199650K .......... .......... .......... .......... .......... 76% 23.0M 7s
199700K .......... .......... .......... .......... .......... 76% 16.9M 7s
199750K .......... .......... .......... .......... .......... 76% 28.6M 6s
199800K .......... .......... .......... .......... .......... 76% 29.0M 6s
199850K .......... .......... .......... .......... .......... 76% 23.9M 6s
199900K .......... .......... .......... .......... .......... 76% 26.9M 6s
199950K .......... .......... .......... .......... .......... 76% 25.6M 6s
200000K .......... .......... .......... .......... .......... 76% 34.9M 6s
200050K .......... .......... .......... .......... .......... 76% 28.7M 6s
200100K .......... .......... .......... .......... .......... 76% 23.0M 6s
200150K .......... .......... .......... .......... .......... 76% 30.0M 6s
200200K .......... .......... .......... .......... .......... 76% 21.7M 6s
200250K .......... .......... .......... .......... .......... 76% 19.4M 6s
200300K .......... .......... .......... .......... .......... 76% 27.2M 6s
200350K .......... .......... .......... .......... .......... 76% 21.4M 6s
200400K .......... .......... .......... .......... .......... 76% 21.5M 6s
200450K .......... .......... .......... .......... .......... 76% 16.4M 6s
200500K .......... .......... .......... .......... .......... 76% 17.6M 6s
200550K .......... .......... .......... .......... .......... 76% 17.6M 6s
200600K .......... .......... .......... .......... .......... 76% 19.5M 6s
200650K .......... .......... .......... .......... .......... 76% 24.6M 6s
200700K .......... .......... .......... .......... .......... 76% 25.3M 6s
200750K .......... .......... .......... .......... .......... 76% 30.6M 6s
200800K .......... .......... .......... .......... .......... 76% 25.2M 6s
200850K .......... .......... .......... .......... .......... 76% 19.6M 6s
200900K .......... .......... .......... .......... .......... 76% 19.1M 6s
200950K .......... .......... .......... .......... .......... 76% 23.6M 6s
201000K .......... .......... .......... .......... .......... 76% 41.6M 6s
201050K .......... .......... .......... .......... .......... 76% 22.5M 6s
201100K .......... .......... .......... .......... .......... 76% 23.0M 6s
201150K .......... .......... .......... .......... .......... 76% 23.9M 6s
201200K .......... .......... .......... .......... .......... 76% 32.5M 6s
201250K .......... .......... .......... .......... .......... 76% 18.5M 6s
201300K .......... .......... .......... .......... .......... 76% 26.3M 6s
201350K .......... .......... .......... .......... .......... 76% 18.4M 6s
201400K .......... .......... .......... .......... .......... 76% 16.2M 6s
201450K .......... .......... .......... .......... .......... 76% 24.2M 6s
201500K .......... .......... .......... .......... .......... 76% 27.7M 6s
201550K .......... .......... .......... .......... .......... 76% 25.1M 6s
201600K .......... .......... .......... .......... .......... 76% 16.7M 6s
201650K .......... .......... .......... .......... .......... 76% 19.7M 6s
201700K .......... .......... .......... .......... .......... 76% 18.7M 6s
201750K .......... .......... .......... .......... .......... 76% 19.7M 6s
201800K .......... .......... .......... .......... .......... 76% 42.9M 6s
201850K .......... .......... .......... .......... .......... 77% 22.2M 6s
201900K .......... .......... .......... .......... .......... 77% 30.5M 6s
201950K .......... .......... .......... .......... .......... 77% 25.0M 6s
202000K .......... .......... .......... .......... .......... 77% 34.9M 6s
202050K .......... .......... .......... .......... .......... 77% 16.3M 6s
202100K .......... .......... .......... .......... .......... 77% 18.1M 6s
202150K .......... .......... .......... .......... .......... 77% 14.2M 6s
202200K .......... .......... .......... .......... .......... 77% 16.7M 6s
202250K .......... .......... .......... .......... .......... 77% 11.4M 6s
202300K .......... .......... .......... .......... .......... 77% 16.1M 6s
202350K .......... .......... .......... .......... .......... 77% 10.6M 6s
202400K .......... .......... .......... .......... .......... 77% 8.93M 6s
202450K .......... .......... .......... .......... .......... 77% 8.44M 6s
202500K .......... .......... .......... .......... .......... 77% 13.9M 6s
202550K .......... .......... .......... .......... .......... 77% 34.4M 6s
202600K .......... .......... .......... .......... .......... 77% 18.4M 6s
202650K .......... .......... .......... .......... .......... 77% 39.6M 6s
202700K .......... .......... .......... .......... .......... 77% 21.3M 6s
202750K .......... .......... .......... .......... .......... 77% 28.2M 6s
202800K .......... .......... .......... .......... .......... 77% 20.5M 6s
202850K .......... .......... .......... .......... .......... 77% 20.1M 6s
202900K .......... .......... .......... .......... .......... 77% 15.9M 6s
202950K .......... .......... .......... .......... .......... 77% 24.3M 6s
203000K .......... .......... .......... .......... .......... 77% 19.0M 6s
203050K .......... .......... .......... .......... .......... 77% 26.5M 6s
203100K .......... .......... .......... .......... .......... 77% 17.3M 6s
203150K .......... .......... .......... .......... .......... 77% 15.5M 6s
203200K .......... .......... .......... .......... .......... 77% 14.9M 6s
203250K .......... .......... .......... .......... .......... 77% 18.9M 6s
203300K .......... .......... .......... .......... .......... 77% 15.1M 6s
203350K .......... .......... .......... .......... .......... 77% 12.6M 6s
203400K .......... .......... .......... .......... .......... 77% 13.5M 6s
203450K .......... .......... .......... .......... .......... 77% 12.7M 6s
203500K .......... .......... .......... .......... .......... 77% 11.0M 6s
203550K .......... .......... .......... .......... .......... 77% 11.2M 6s
203600K .......... .......... .......... .......... .......... 77% 10.7M 6s
203650K .......... .......... .......... .......... .......... 77% 15.6M 6s
203700K .......... .......... .......... .......... .......... 77% 16.8M 6s
203750K .......... .......... .......... .......... .......... 77% 18.4M 6s
203800K .......... .......... .......... .......... .......... 77% 15.9M 6s
203850K .......... .......... .......... .......... .......... 77% 12.3M 6s
203900K .......... .......... .......... .......... .......... 77% 14.3M 6s
203950K .......... .......... .......... .......... .......... 77% 12.6M 6s
204000K .......... .......... .......... .......... .......... 77% 26.6M 6s
204050K .......... .......... .......... .......... .......... 77% 12.7M 6s
204100K .......... .......... .......... .......... .......... 77% 13.8M 6s
204150K .......... .......... .......... .......... .......... 77% 10.2M 6s
204200K .......... .......... .......... .......... .......... 77% 16.1M 6s
204250K .......... .......... .......... .......... .......... 77% 26.5M 6s
204300K .......... .......... .......... .......... .......... 77% 21.1M 6s
204350K .......... .......... .......... .......... .......... 77% 17.7M 6s
204400K .......... .......... .......... .......... .......... 77% 19.0M 6s
204450K .......... .......... .......... .......... .......... 77% 18.7M 6s
204500K .......... .......... .......... .......... .......... 78% 19.8M 6s
204550K .......... .......... .......... .......... .......... 78% 23.5M 6s
204600K .......... .......... .......... .......... .......... 78% 14.5M 6s
204650K .......... .......... .......... .......... .......... 78% 17.8M 6s
204700K .......... .......... .......... .......... .......... 78% 17.3M 6s
204750K .......... .......... .......... .......... .......... 78% 14.4M 6s
204800K .......... .......... .......... .......... .......... 78% 12.4M 6s
204850K .......... .......... .......... .......... .......... 78% 10.8M 6s
204900K .......... .......... .......... .......... .......... 78% 12.7M 6s
204950K .......... .......... .......... .......... .......... 78% 11.1M 6s
205000K .......... .......... .......... .......... .......... 78% 9.86M 6s
205050K .......... .......... .......... .......... .......... 78% 18.1M 6s
205100K .......... .......... .......... .......... .......... 78% 17.4M 6s
205150K .......... .......... .......... .......... .......... 78% 17.0M 6s
205200K .......... .......... .......... .......... .......... 78% 9.33M 6s
205250K .......... .......... .......... .......... .......... 78% 18.4M 6s
205300K .......... .......... .......... .......... .......... 78% 16.5M 6s
205350K .......... .......... .......... .......... .......... 78% 14.5M 6s
205400K .......... .......... .......... .......... .......... 78% 17.1M 6s
205450K .......... .......... .......... .......... .......... 78% 19.8M 6s
205500K .......... .......... .......... .......... .......... 78% 16.5M 6s
205550K .......... .......... .......... .......... .......... 78% 18.5M 6s
205600K .......... .......... .......... .......... .......... 78% 11.5M 6s
205650K .......... .......... .......... .......... .......... 78% 15.2M 6s
205700K .......... .......... .......... .......... .......... 78% 11.2M 6s
205750K .......... .......... .......... .......... .......... 78% 15.9M 6s
205800K .......... .......... .......... .......... .......... 78% 18.0M 6s
205850K .......... .......... .......... .......... .......... 78% 8.63M 6s
205900K .......... .......... .......... .......... .......... 78% 10.2M 6s
205950K .......... .......... .......... .......... .......... 78% 12.3M 6s
206000K .......... .......... .......... .......... .......... 78% 23.6M 6s
206050K .......... .......... .......... .......... .......... 78% 20.8M 6s
206100K .......... .......... .......... .......... .......... 78% 15.4M 6s
206150K .......... .......... .......... .......... .......... 78% 22.8M 6s
206200K .......... .......... .......... .......... .......... 78% 17.2M 6s
206250K .......... .......... .......... .......... .......... 78% 18.5M 6s
206300K .......... .......... .......... .......... .......... 78% 19.2M 6s
206350K .......... .......... .......... .......... .......... 78% 19.7M 6s
206400K .......... .......... .......... .......... .......... 78% 24.4M 6s
206450K .......... .......... .......... .......... .......... 78% 15.0M 6s
206500K .......... .......... .......... .......... .......... 78% 15.1M 6s
206550K .......... .......... .......... .......... .......... 78% 10.8M 6s
206600K .......... .......... .......... .......... .......... 78% 9.29M 6s
206650K .......... .......... .......... .......... .......... 78% 17.7M 6s
206700K .......... .......... .......... .......... .......... 78% 8.23M 6s
206750K .......... .......... .......... .......... .......... 78% 10.8M 6s
206800K .......... .......... .......... .......... .......... 78% 10.8M 6s
206850K .......... .......... .......... .......... .......... 78% 8.72M 6s
206900K .......... .......... .......... .......... .......... 78% 13.3M 6s
206950K .......... .......... .......... .......... .......... 78% 13.7M 6s
207000K .......... .......... .......... .......... .......... 78% 11.3M 6s
207050K .......... .......... .......... .......... .......... 78% 7.43M 6s
207100K .......... .......... .......... .......... .......... 79% 11.7M 6s
207150K .......... .......... .......... .......... .......... 79% 22.4M 6s
207200K .......... .......... .......... .......... .......... 79% 10.8M 6s
207250K .......... .......... .......... .......... .......... 79% 13.0M 6s
207300K .......... .......... .......... .......... .......... 79% 31.9M 6s
207350K .......... .......... .......... .......... .......... 79% 15.8M 6s
207400K .......... .......... .......... .......... .......... 79% 13.9M 6s
207450K .......... .......... .......... .......... .......... 79% 13.9M 6s
207500K .......... .......... .......... .......... .......... 79% 16.5M 6s
207550K .......... .......... .......... .......... .......... 79% 19.9M 6s
207600K .......... .......... .......... .......... .......... 79% 17.4M 6s
207650K .......... .......... .......... .......... .......... 79% 30.9M 6s
207700K .......... .......... .......... .......... .......... 79% 22.2M 6s
207750K .......... .......... .......... .......... .......... 79% 11.6M 6s
207800K .......... .......... .......... .......... .......... 79% 39.1M 6s
207850K .......... .......... .......... .......... .......... 79% 14.2M 6s
207900K .......... .......... .......... .......... .......... 79% 16.0M 6s
207950K .......... .......... .......... .......... .......... 79% 12.2M 6s
208000K .......... .......... .......... .......... .......... 79% 23.8M 6s
208050K .......... .......... .......... .......... .......... 79% 22.2M 6s
208100K .......... .......... .......... .......... .......... 79% 14.3M 6s
208150K .......... .......... .......... .......... .......... 79% 21.9M 6s
208200K .......... .......... .......... .......... .......... 79% 12.6M 6s
208250K .......... .......... .......... .......... .......... 79% 23.4M 6s
208300K .......... .......... .......... .......... .......... 79% 22.4M 6s
208350K .......... .......... .......... .......... .......... 79% 26.2M 5s
208400K .......... .......... .......... .......... .......... 79% 26.8M 5s
208450K .......... .......... .......... .......... .......... 79% 19.7M 5s
208500K .......... .......... .......... .......... .......... 79% 27.3M 5s
208550K .......... .......... .......... .......... .......... 79% 18.8M 5s
208600K .......... .......... .......... .......... .......... 79% 21.2M 5s
208650K .......... .......... .......... .......... .......... 79% 15.2M 5s
208700K .......... .......... .......... .......... .......... 79% 14.8M 5s
208750K .......... .......... .......... .......... .......... 79% 16.8M 5s
208800K .......... .......... .......... .......... .......... 79% 15.0M 5s
208850K .......... .......... .......... .......... .......... 79% 16.8M 5s
208900K .......... .......... .......... .......... .......... 79% 17.3M 5s
208950K .......... .......... .......... .......... .......... 79% 10.3M 5s
209000K .......... .......... .......... .......... .......... 79% 12.4M 5s
209050K .......... .......... .......... .......... .......... 79% 12.7M 5s
209100K .......... .......... .......... .......... .......... 79% 9.72M 5s
209150K .......... .......... .......... .......... .......... 79% 13.3M 5s
209200K .......... .......... .......... .......... .......... 79% 7.99M 5s
209250K .......... .......... .......... .......... .......... 79% 7.04M 5s
209300K .......... .......... .......... .......... .......... 79% 9.73M 5s
209350K .......... .......... .......... .......... .......... 79% 7.18M 5s
209400K .......... .......... .......... .......... .......... 79% 11.4M 5s
209450K .......... .......... .......... .......... .......... 79% 9.38M 5s
209500K .......... .......... .......... .......... .......... 79% 8.31M 5s
209550K .......... .......... .......... .......... .......... 79% 5.28M 5s
209600K .......... .......... .......... .......... .......... 79% 8.24M 5s
209650K .......... .......... .......... .......... .......... 79% 10.8M 5s
209700K .......... .......... .......... .......... .......... 79% 8.98M 5s
209750K .......... .......... .......... .......... .......... 80% 11.6M 5s
209800K .......... .......... .......... .......... .......... 80% 11.3M 5s
209850K .......... .......... .......... .......... .......... 80% 10.9M 5s
209900K .......... .......... .......... .......... .......... 80% 14.5M 5s
209950K .......... .......... .......... .......... .......... 80% 8.41M 5s
210000K .......... .......... .......... .......... .......... 80% 8.44M 5s
210050K .......... .......... .......... .......... .......... 80% 12.7M 5s
210100K .......... .......... .......... .......... .......... 80% 12.9M 5s
210150K .......... .......... .......... .......... .......... 80% 21.7M 5s
210200K .......... .......... .......... .......... .......... 80% 12.4M 5s
210250K .......... .......... .......... .......... .......... 80% 11.6M 5s
210300K .......... .......... .......... .......... .......... 80% 20.2M 5s
210350K .......... .......... .......... .......... .......... 80% 16.7M 5s
210400K .......... .......... .......... .......... .......... 80% 19.1M 5s
210450K .......... .......... .......... .......... .......... 80% 16.7M 5s
210500K .......... .......... .......... .......... .......... 80% 19.3M 5s
210550K .......... .......... .......... .......... .......... 80% 18.6M 5s
210600K .......... .......... .......... .......... .......... 80% 11.2M 5s
210650K .......... .......... .......... .......... .......... 80% 15.3M 5s
210700K .......... .......... .......... .......... .......... 80% 14.3M 5s
210750K .......... .......... .......... .......... .......... 80% 16.6M 5s
210800K .......... .......... .......... .......... .......... 80% 15.1M 5s
210850K .......... .......... .......... .......... .......... 80% 13.9M 5s
210900K .......... .......... .......... .......... .......... 80% 13.1M 5s
210950K .......... .......... .......... .......... .......... 80% 11.7M 5s
211000K .......... .......... .......... .......... .......... 80% 12.2M 5s
211050K .......... .......... .......... .......... .......... 80% 8.48M 5s
211100K .......... .......... .......... .......... .......... 80% 7.40M 5s
211150K .......... .......... .......... .......... .......... 80% 7.62M 5s
211200K .......... .......... .......... .......... .......... 80% 5.35M 5s
211250K .......... .......... .......... .......... .......... 80% 7.41M 5s
211300K .......... .......... .......... .......... .......... 80% 8.51M 5s
211350K .......... .......... .......... .......... .......... 80% 7.37M 5s
211400K .......... .......... .......... .......... .......... 80% 6.75M 5s
211450K .......... .......... .......... .......... .......... 80% 9.46M 5s
211500K .......... .......... .......... .......... .......... 80% 8.54M 5s
211550K .......... .......... .......... .......... .......... 80% 10.9M 5s
211600K .......... .......... .......... .......... .......... 80% 9.08M 5s
211650K .......... .......... .......... .......... .......... 80% 10.8M 5s
211700K .......... .......... .......... .......... .......... 80% 12.9M 5s
211750K .......... .......... .......... .......... .......... 80% 13.3M 5s
211800K .......... .......... .......... .......... .......... 80% 18.8M 5s
211850K .......... .......... .......... .......... .......... 80% 13.6M 5s
211900K .......... .......... .......... .......... .......... 80% 9.30M 5s
211950K .......... .......... .......... .......... .......... 80% 9.15M 5s
212000K .......... .......... .......... .......... .......... 80% 8.01M 5s
212050K .......... .......... .......... .......... .......... 80% 9.14M 5s
212100K .......... .......... .......... .......... .......... 80% 7.29M 5s
212150K .......... .......... .......... .......... .......... 80% 4.98M 5s
212200K .......... .......... .......... .......... .......... 80% 3.72M 5s
212250K .......... .......... .......... .......... .......... 80% 1.72M 5s
212300K .......... .......... .......... .......... .......... 80% 1.77M 5s
212350K .......... .......... .......... .......... .......... 81% 3.09M 5s
212400K .......... .......... .......... .......... .......... 81% 4.54M 5s
212450K .......... .......... .......... .......... .......... 81% 1.60M 5s
212500K .......... .......... .......... .......... .......... 81% 9.93M 5s
212550K .......... .......... .......... .......... .......... 81% 10.0M 5s
212600K .......... .......... .......... .......... .......... 81% 10.5M 5s
212650K .......... .......... .......... .......... .......... 81% 11.8M 5s
212700K .......... .......... .......... .......... .......... 81% 10.3M 5s
212750K .......... .......... .......... .......... .......... 81% 8.51M 5s
212800K .......... .......... .......... .......... .......... 81% 8.60M 5s
212850K .......... .......... .......... .......... .......... 81% 7.27M 5s
212900K .......... .......... .......... .......... .......... 81% 5.98M 5s
212950K .......... .......... .......... .......... .......... 81% 4.37M 5s
213000K .......... .......... .......... .......... .......... 81% 5.07M 5s
213050K .......... .......... .......... .......... .......... 81% 10.4M 5s
213100K .......... .......... .......... .......... .......... 81% 5.60M 5s
213150K .......... .......... .......... .......... .......... 81% 16.5M 5s
213200K .......... .......... .......... .......... .......... 81% 5.23M 5s
213250K .......... .......... .......... .......... .......... 81% 14.0M 5s
213300K .......... .......... .......... .......... .......... 81% 10.1M 5s
213350K .......... .......... .......... .......... .......... 81% 15.4M 5s
213400K .......... .......... .......... .......... .......... 81% 13.9M 5s
213450K .......... .......... .......... .......... .......... 81% 12.8M 5s
213500K .......... .......... .......... .......... .......... 81% 15.3M 5s
213550K .......... .......... .......... .......... .......... 81% 18.4M 5s
213600K .......... .......... .......... .......... .......... 81% 14.1M 5s
213650K .......... .......... .......... .......... .......... 81% 16.9M 5s
213700K .......... .......... .......... .......... .......... 81% 11.6M 5s
213750K .......... .......... .......... .......... .......... 81% 13.3M 5s
213800K .......... .......... .......... .......... .......... 81% 12.9M 5s
213850K .......... .......... .......... .......... .......... 81% 9.56M 5s
213900K .......... .......... .......... .......... .......... 81% 8.18M 5s
213950K .......... .......... .......... .......... .......... 81% 9.20M 5s
214000K .......... .......... .......... .......... .......... 81% 9.73M 5s
214050K .......... .......... .......... .......... .......... 81% 9.01M 5s
214100K .......... .......... .......... .......... .......... 81% 5.59M 5s
214150K .......... .......... .......... .......... .......... 81% 7.16M 5s
214200K .......... .......... .......... .......... .......... 81% 6.50M 5s
214250K .......... .......... .......... .......... .......... 81% 7.99M 5s
214300K .......... .......... .......... .......... .......... 81% 12.9M 5s
214350K .......... .......... .......... .......... .......... 81% 13.4M 5s
214400K .......... .......... .......... .......... .......... 81% 11.7M 5s
214450K .......... .......... .......... .......... .......... 81% 9.25M 5s
214500K .......... .......... .......... .......... .......... 81% 14.5M 5s
214550K .......... .......... .......... .......... .......... 81% 14.5M 5s
214600K .......... .......... .......... .......... .......... 81% 14.1M 5s
214650K .......... .......... .......... .......... .......... 81% 6.85M 5s
214700K .......... .......... .......... .......... .......... 81% 6.30M 5s
214750K .......... .......... .......... .......... .......... 81% 7.92M 5s
214800K .......... .......... .......... .......... .......... 81% 7.45M 5s
214850K .......... .......... .......... .......... .......... 81% 5.39M 5s
214900K .......... .......... .......... .......... .......... 81% 4.67M 5s
214950K .......... .......... .......... .......... .......... 81% 4.01M 5s
215000K .......... .......... .......... .......... .......... 82% 2.03M 5s
215050K .......... .......... .......... .......... .......... 82% 18.4M 5s
215100K .......... .......... .......... .......... .......... 82% 10.7M 5s
215150K .......... .......... .......... .......... .......... 82% 15.1M 5s
215200K .......... .......... .......... .......... .......... 82% 9.74M 5s
215250K .......... .......... .......... .......... .......... 82% 10.5M 5s
215300K .......... .......... .......... .......... .......... 82% 22.6M 5s
215350K .......... .......... .......... .......... .......... 82% 18.0M 5s
215400K .......... .......... .......... .......... .......... 82% 18.6M 5s
215450K .......... .......... .......... .......... .......... 82% 18.1M 5s
215500K .......... .......... .......... .......... .......... 82% 22.8M 5s
215550K .......... .......... .......... .......... .......... 82% 21.2M 5s
215600K .......... .......... .......... .......... .......... 82% 16.3M 5s
215650K .......... .......... .......... .......... .......... 82% 22.2M 5s
215700K .......... .......... .......... .......... .......... 82% 17.1M 5s
215750K .......... .......... .......... .......... .......... 82% 16.3M 5s
215800K .......... .......... .......... .......... .......... 82% 10.3M 5s
215850K .......... .......... .......... .......... .......... 82% 13.6M 5s
215900K .......... .......... .......... .......... .......... 82% 14.7M 5s
215950K .......... .......... .......... .......... .......... 82% 10.1M 5s
216000K .......... .......... .......... .......... .......... 82% 17.0M 5s
216050K .......... .......... .......... .......... .......... 82% 12.8M 5s
216100K .......... .......... .......... .......... .......... 82% 8.68M 5s
216150K .......... .......... .......... .......... .......... 82% 12.9M 5s
216200K .......... .......... .......... .......... .......... 82% 15.0M 5s
216250K .......... .......... .......... .......... .......... 82% 18.9M 5s
216300K .......... .......... .......... .......... .......... 82% 20.9M 5s
216350K .......... .......... .......... .......... .......... 82% 14.9M 5s
216400K .......... .......... .......... .......... .......... 82% 19.9M 5s
216450K .......... .......... .......... .......... .......... 82% 18.7M 5s
216500K .......... .......... .......... .......... .......... 82% 18.9M 5s
216550K .......... .......... .......... .......... .......... 82% 20.7M 5s
216600K .......... .......... .......... .......... .......... 82% 16.5M 5s
216650K .......... .......... .......... .......... .......... 82% 13.3M 5s
216700K .......... .......... .......... .......... .......... 82% 15.5M 5s
216750K .......... .......... .......... .......... .......... 82% 19.3M 5s
216800K .......... .......... .......... .......... .......... 82% 12.7M 5s
216850K .......... .......... .......... .......... .......... 82% 11.7M 5s
216900K .......... .......... .......... .......... .......... 82% 11.2M 5s
216950K .......... .......... .......... .......... .......... 82% 10.5M 5s
217000K .......... .......... .......... .......... .......... 82% 17.5M 5s
217050K .......... .......... .......... .......... .......... 82% 16.8M 5s
217100K .......... .......... .......... .......... .......... 82% 15.3M 5s
217150K .......... .......... .......... .......... .......... 82% 15.9M 5s
217200K .......... .......... .......... .......... .......... 82% 11.2M 5s
217250K .......... .......... .......... .......... .......... 82% 12.0M 5s
217300K .......... .......... .......... .......... .......... 82% 9.90M 5s
217350K .......... .......... .......... .......... .......... 82% 12.0M 5s
217400K .......... .......... .......... .......... .......... 82% 15.2M 5s
217450K .......... .......... .......... .......... .......... 82% 12.4M 5s
217500K .......... .......... .......... .......... .......... 82% 14.7M 5s
217550K .......... .......... .......... .......... .......... 82% 10.8M 5s
217600K .......... .......... .......... .......... .......... 83% 8.55M 5s
217650K .......... .......... .......... .......... .......... 83% 11.7M 5s
217700K .......... .......... .......... .......... .......... 83% 11.4M 5s
217750K .......... .......... .......... .......... .......... 83% 10.2M 5s
217800K .......... .......... .......... .......... .......... 83% 11.7M 5s
217850K .......... .......... .......... .......... .......... 83% 9.81M 5s
217900K .......... .......... .......... .......... .......... 83% 12.2M 5s
217950K .......... .......... .......... .......... .......... 83% 8.43M 5s
218000K .......... .......... .......... .......... .......... 83% 10.2M 5s
218050K .......... .......... .......... .......... .......... 83% 7.38M 5s
218100K .......... .......... .......... .......... .......... 83% 6.06M 5s
218150K .......... .......... .......... .......... .......... 83% 6.29M 4s
218200K .......... .......... .......... .......... .......... 83% 6.74M 4s
218250K .......... .......... .......... .......... .......... 83% 6.25M 4s
218300K .......... .......... .......... .......... .......... 83% 13.6M 4s
218350K .......... .......... .......... .......... .......... 83% 10.0M 4s
218400K .......... .......... .......... .......... .......... 83% 11.8M 4s
218450K .......... .......... .......... .......... .......... 83% 9.54M 4s
218500K .......... .......... .......... .......... .......... 83% 15.0M 4s
218550K .......... .......... .......... .......... .......... 83% 12.3M 4s
218600K .......... .......... .......... .......... .......... 83% 8.00M 4s
218650K .......... .......... .......... .......... .......... 83% 10.9M 4s
218700K .......... .......... .......... .......... .......... 83% 9.31M 4s
218750K .......... .......... .......... .......... .......... 83% 14.5M 4s
218800K .......... .......... .......... .......... .......... 83% 11.0M 4s
218850K .......... .......... .......... .......... .......... 83% 9.29M 4s
218900K .......... .......... .......... .......... .......... 83% 11.6M 4s
218950K .......... .......... .......... .......... .......... 83% 17.8M 4s
219000K .......... .......... .......... .......... .......... 83% 11.9M 4s
219050K .......... .......... .......... .......... .......... 83% 10.2M 4s
219100K .......... .......... .......... .......... .......... 83% 8.72M 4s
219150K .......... .......... .......... .......... .......... 83% 11.8M 4s
219200K .......... .......... .......... .......... .......... 83% 7.92M 4s
219250K .......... .......... .......... .......... .......... 83% 8.40M 4s
219300K .......... .......... .......... .......... .......... 83% 12.6M 4s
219350K .......... .......... .......... .......... .......... 83% 9.83M 4s
219400K .......... .......... .......... .......... .......... 83% 11.1M 4s
219450K .......... .......... .......... .......... .......... 83% 12.2M 4s
219500K .......... .......... .......... .......... .......... 83% 10.7M 4s
219550K .......... .......... .......... .......... .......... 83% 7.19M 4s
219600K .......... .......... .......... .......... .......... 83% 6.20M 4s
219650K .......... .......... .......... .......... .......... 83% 10.3M 4s
219700K .......... .......... .......... .......... .......... 83% 8.50M 4s
219750K .......... .......... .......... .......... .......... 83% 13.0M 4s
219800K .......... .......... .......... .......... .......... 83% 8.41M 4s
219850K .......... .......... .......... .......... .......... 83% 9.19M 4s
219900K .......... .......... .......... .......... .......... 83% 13.8M 4s
219950K .......... .......... .......... .......... .......... 83% 9.10M 4s
220000K .......... .......... .......... .......... .......... 83% 12.4M 4s
220050K .......... .......... .......... .......... .......... 83% 13.2M 4s
220100K .......... .......... .......... .......... .......... 83% 15.3M 4s
220150K .......... .......... .......... .......... .......... 83% 10.6M 4s
220200K .......... .......... .......... .......... .......... 84% 9.39M 4s
220250K .......... .......... .......... .......... .......... 84% 11.8M 4s
220300K .......... .......... .......... .......... .......... 84% 8.41M 4s
220350K .......... .......... .......... .......... .......... 84% 5.54M 4s
220400K .......... .......... .......... .......... .......... 84% 14.4M 4s
220450K .......... .......... .......... .......... .......... 84% 8.87M 4s
220500K .......... .......... .......... .......... .......... 84% 14.0M 4s
220550K .......... .......... .......... .......... .......... 84% 14.1M 4s
220600K .......... .......... .......... .......... .......... 84% 9.35M 4s
220650K .......... .......... .......... .......... .......... 84% 12.5M 4s
220700K .......... .......... .......... .......... .......... 84% 13.0M 4s
220750K .......... .......... .......... .......... .......... 84% 14.9M 4s
220800K .......... .......... .......... .......... .......... 84% 20.3M 4s
220850K .......... .......... .......... .......... .......... 84% 12.6M 4s
220900K .......... .......... .......... .......... .......... 84% 19.7M 4s
220950K .......... .......... .......... .......... .......... 84% 8.87M 4s
221000K .......... .......... .......... .......... .......... 84% 14.2M 4s
221050K .......... .......... .......... .......... .......... 84% 12.7M 4s
221100K .......... .......... .......... .......... .......... 84% 12.7M 4s
221150K .......... .......... .......... .......... .......... 84% 14.8M 4s
221200K .......... .......... .......... .......... .......... 84% 14.0M 4s
221250K .......... .......... .......... .......... .......... 84% 17.5M 4s
221300K .......... .......... .......... .......... .......... 84% 14.8M 4s
221350K .......... .......... .......... .......... .......... 84% 11.6M 4s
221400K .......... .......... .......... .......... .......... 84% 17.2M 4s
221450K .......... .......... .......... .......... .......... 84% 12.3M 4s
221500K .......... .......... .......... .......... .......... 84% 15.1M 4s
221550K .......... .......... .......... .......... .......... 84% 11.8M 4s
221600K .......... .......... .......... .......... .......... 84% 12.4M 4s
221650K .......... .......... .......... .......... .......... 84% 15.3M 4s
221700K .......... .......... .......... .......... .......... 84% 9.46M 4s
221750K .......... .......... .......... .......... .......... 84% 8.84M 4s
221800K .......... .......... .......... .......... .......... 84% 8.62M 4s
221850K .......... .......... .......... .......... .......... 84% 7.24M 4s
221900K .......... .......... .......... .......... .......... 84% 8.14M 4s
221950K .......... .......... .......... .......... .......... 84% 6.25M 4s
222000K .......... .......... .......... .......... .......... 84% 12.3M 4s
222050K .......... .......... .......... .......... .......... 84% 13.7M 4s
222100K .......... .......... .......... .......... .......... 84% 15.4M 4s
222150K .......... .......... .......... .......... .......... 84% 15.8M 4s
222200K .......... .......... .......... .......... .......... 84% 7.10M 4s
222250K .......... .......... .......... .......... .......... 84% 11.1M 4s
222300K .......... .......... .......... .......... .......... 84% 9.44M 4s
222350K .......... .......... .......... .......... .......... 84% 8.46M 4s
222400K .......... .......... .......... .......... .......... 84% 7.30M 4s
222450K .......... .......... .......... .......... .......... 84% 13.9M 4s
222500K .......... .......... .......... .......... .......... 84% 17.1M 4s
222550K .......... .......... .......... .......... .......... 84% 15.8M 4s
222600K .......... .......... .......... .......... .......... 84% 14.4M 4s
222650K .......... .......... .......... .......... .......... 84% 19.1M 4s
222700K .......... .......... .......... .......... .......... 84% 12.7M 4s
222750K .......... .......... .......... .......... .......... 84% 17.8M 4s
222800K .......... .......... .......... .......... .......... 84% 16.6M 4s
222850K .......... .......... .......... .......... .......... 85% 16.1M 4s
222900K .......... .......... .......... .......... .......... 85% 14.3M 4s
222950K .......... .......... .......... .......... .......... 85% 10.2M 4s
223000K .......... .......... .......... .......... .......... 85% 12.6M 4s
223050K .......... .......... .......... .......... .......... 85% 11.7M 4s
223100K .......... .......... .......... .......... .......... 85% 9.97M 4s
223150K .......... .......... .......... .......... .......... 85% 14.9M 4s
223200K .......... .......... .......... .......... .......... 85% 7.48M 4s
223250K .......... .......... .......... .......... .......... 85% 15.0M 4s
223300K .......... .......... .......... .......... .......... 85% 22.5M 4s
223350K .......... .......... .......... .......... .......... 85% 11.1M 4s
223400K .......... .......... .......... .......... .......... 85% 12.9M 4s
223450K .......... .......... .......... .......... .......... 85% 20.4M 4s
223500K .......... .......... .......... .......... .......... 85% 15.9M 4s
223550K .......... .......... .......... .......... .......... 85% 34.1M 4s
223600K .......... .......... .......... .......... .......... 85% 14.3M 4s
223650K .......... .......... .......... .......... .......... 85% 13.2M 4s
223700K .......... .......... .......... .......... .......... 85% 31.7M 4s
223750K .......... .......... .......... .......... .......... 85% 21.0M 4s
223800K .......... .......... .......... .......... .......... 85% 27.6M 4s
223850K .......... .......... .......... .......... .......... 85% 14.0M 4s
223900K .......... .......... .......... .......... .......... 85% 21.2M 4s
223950K .......... .......... .......... .......... .......... 85% 16.1M 4s
224000K .......... .......... .......... .......... .......... 85% 16.1M 4s
224050K .......... .......... .......... .......... .......... 85% 17.2M 4s
224100K .......... .......... .......... .......... .......... 85% 14.6M 4s
224150K .......... .......... .......... .......... .......... 85% 14.1M 4s
224200K .......... .......... .......... .......... .......... 85% 17.1M 4s
224250K .......... .......... .......... .......... .......... 85% 13.1M 4s
224300K .......... .......... .......... .......... .......... 85% 9.97M 4s
224350K .......... .......... .......... .......... .......... 85% 8.07M 4s
224400K .......... .......... .......... .......... .......... 85% 8.72M 4s
224450K .......... .......... .......... .......... .......... 85% 6.14M 4s
224500K .......... .......... .......... .......... .......... 85% 15.8M 4s
224550K .......... .......... .......... .......... .......... 85% 11.9M 4s
224600K .......... .......... .......... .......... .......... 85% 10.4M 4s
224650K .......... .......... .......... .......... .......... 85% 15.3M 4s
224700K .......... .......... .......... .......... .......... 85% 8.36M 4s
224750K .......... .......... .......... .......... .......... 85% 12.7M 4s
224800K .......... .......... .......... .......... .......... 85% 14.4M 4s
224850K .......... .......... .......... .......... .......... 85% 13.1M 4s
224900K .......... .......... .......... .......... .......... 85% 14.5M 4s
224950K .......... .......... .......... .......... .......... 85% 7.01M 4s
225000K .......... .......... .......... .......... .......... 85% 11.7M 4s
225050K .......... .......... .......... .......... .......... 85% 13.1M 4s
225100K .......... .......... .......... .......... .......... 85% 11.8M 4s
225150K .......... .......... .......... .......... .......... 85% 12.2M 4s
225200K .......... .......... .......... .......... .......... 85% 8.23M 4s
225250K .......... .......... .......... .......... .......... 85% 24.2M 4s
225300K .......... .......... .......... .......... .......... 85% 20.3M 4s
225350K .......... .......... .......... .......... .......... 85% 16.1M 4s
225400K .......... .......... .......... .......... .......... 85% 18.1M 4s
225450K .......... .......... .......... .......... .......... 86% 11.5M 4s
225500K .......... .......... .......... .......... .......... 86% 8.15M 4s
225550K .......... .......... .......... .......... .......... 86% 13.6M 4s
225600K .......... .......... .......... .......... .......... 86% 10.7M 4s
225650K .......... .......... .......... .......... .......... 86% 12.8M 4s
225700K .......... .......... .......... .......... .......... 86% 11.9M 4s
225750K .......... .......... .......... .......... .......... 86% 18.0M 4s
225800K .......... .......... .......... .......... .......... 86% 14.2M 4s
225850K .......... .......... .......... .......... .......... 86% 15.2M 4s
225900K .......... .......... .......... .......... .......... 86% 11.5M 4s
225950K .......... .......... .......... .......... .......... 86% 7.18M 4s
226000K .......... .......... .......... .......... .......... 86% 9.42M 4s
226050K .......... .......... .......... .......... .......... 86% 9.67M 4s
226100K .......... .......... .......... .......... .......... 86% 9.38M 4s
226150K .......... .......... .......... .......... .......... 86% 4.72M 4s
226200K .......... .......... .......... .......... .......... 86% 3.94M 4s
226250K .......... .......... .......... .......... .......... 86% 5.40M 4s
226300K .......... .......... .......... .......... .......... 86% 7.46M 4s
226350K .......... .......... .......... .......... .......... 86% 11.0M 4s
226400K .......... .......... .......... .......... .......... 86% 21.5M 4s
226450K .......... .......... .......... .......... .......... 86% 9.47M 4s
226500K .......... .......... .......... .......... .......... 86% 9.04M 4s
226550K .......... .......... .......... .......... .......... 86% 18.3M 4s
226600K .......... .......... .......... .......... .......... 86% 13.0M 4s
226650K .......... .......... .......... .......... .......... 86% 12.2M 4s
226700K .......... .......... .......... .......... .......... 86% 17.2M 4s
226750K .......... .......... .......... .......... .......... 86% 10.9M 4s
226800K .......... .......... .......... .......... .......... 86% 67.8M 4s
226850K .......... .......... .......... .......... .......... 86% 20.1M 4s
226900K .......... .......... .......... .......... .......... 86% 25.3M 4s
226950K .......... .......... .......... .......... .......... 86% 14.7M 4s
227000K .......... .......... .......... .......... .......... 86% 17.5M 4s
227050K .......... .......... .......... .......... .......... 86% 18.3M 4s
227100K .......... .......... .......... .......... .......... 86% 18.0M 4s
227150K .......... .......... .......... .......... .......... 86% 14.5M 4s
227200K .......... .......... .......... .......... .......... 86% 12.2M 4s
227250K .......... .......... .......... .......... .......... 86% 17.2M 4s
227300K .......... .......... .......... .......... .......... 86% 17.5M 4s
227350K .......... .......... .......... .......... .......... 86% 11.7M 4s
227400K .......... .......... .......... .......... .......... 86% 19.4M 4s
227450K .......... .......... .......... .......... .......... 86% 12.4M 4s
227500K .......... .......... .......... .......... .......... 86% 12.7M 4s
227550K .......... .......... .......... .......... .......... 86% 10.3M 4s
227600K .......... .......... .......... .......... .......... 86% 7.64M 4s
227650K .......... .......... .......... .......... .......... 86% 14.0M 4s
227700K .......... .......... .......... .......... .......... 86% 9.16M 3s
227750K .......... .......... .......... .......... .......... 86% 11.0M 3s
227800K .......... .......... .......... .......... .......... 86% 14.2M 3s
227850K .......... .......... .......... .......... .......... 86% 14.5M 3s
227900K .......... .......... .......... .......... .......... 86% 25.0M 3s
227950K .......... .......... .......... .......... .......... 86% 20.8M 3s
228000K .......... .......... .......... .......... .......... 86% 20.7M 3s
228050K .......... .......... .......... .......... .......... 86% 24.0M 3s
228100K .......... .......... .......... .......... .......... 87% 14.8M 3s
228150K .......... .......... .......... .......... .......... 87% 25.2M 3s
228200K .......... .......... .......... .......... .......... 87% 14.0M 3s
228250K .......... .......... .......... .......... .......... 87% 16.7M 3s
228300K .......... .......... .......... .......... .......... 87% 23.3M 3s
228350K .......... .......... .......... .......... .......... 87% 14.1M 3s
228400K .......... .......... .......... .......... .......... 87% 21.1M 3s
228450K .......... .......... .......... .......... .......... 87% 19.4M 3s
228500K .......... .......... .......... .......... .......... 87% 25.2M 3s
228550K .......... .......... .......... .......... .......... 87% 24.8M 3s
228600K .......... .......... .......... .......... .......... 87% 28.7M 3s
228650K .......... .......... .......... .......... .......... 87% 17.6M 3s
228700K .......... .......... .......... .......... .......... 87% 22.7M 3s
228750K .......... .......... .......... .......... .......... 87% 9.48M 3s
228800K .......... .......... .......... .......... .......... 87% 10.7M 3s
228850K .......... .......... .......... .......... .......... 87% 7.61M 3s
228900K .......... .......... .......... .......... .......... 87% 9.18M 3s
228950K .......... .......... .......... .......... .......... 87% 6.98M 3s
229000K .......... .......... .......... .......... .......... 87% 8.56M 3s
229050K .......... .......... .......... .......... .......... 87% 7.51M 3s
229100K .......... .......... .......... .......... .......... 87% 10.2M 3s
229150K .......... .......... .......... .......... .......... 87% 27.8M 3s
229200K .......... .......... .......... .......... .......... 87% 10.1M 3s
229250K .......... .......... .......... .......... .......... 87% 65.4M 3s
229300K .......... .......... .......... .......... .......... 87% 15.1M 3s
229350K .......... .......... .......... .......... .......... 87% 14.7M 3s
229400K .......... .......... .......... .......... .......... 87% 18.5M 3s
229450K .......... .......... .......... .......... .......... 87% 17.5M 3s
229500K .......... .......... .......... .......... .......... 87% 19.3M 3s
229550K .......... .......... .......... .......... .......... 87% 15.7M 3s
229600K .......... .......... .......... .......... .......... 87% 10.1M 3s
229650K .......... .......... .......... .......... .......... 87% 10.1M 3s
229700K .......... .......... .......... .......... .......... 87% 5.92M 3s
229750K .......... .......... .......... .......... .......... 87% 4.87M 3s
229800K .......... .......... .......... .......... .......... 87% 7.73M 3s
229850K .......... .......... .......... .......... .......... 87% 5.61M 3s
229900K .......... .......... .......... .......... .......... 87% 12.0M 3s
229950K .......... .......... .......... .......... .......... 87% 7.38M 3s
230000K .......... .......... .......... .......... .......... 87% 15.5M 3s
230050K .......... .......... .......... .......... .......... 87% 28.8M 3s
230100K .......... .......... .......... .......... .......... 87% 16.2M 3s
230150K .......... .......... .......... .......... .......... 87% 15.0M 3s
230200K .......... .......... .......... .......... .......... 87% 18.7M 3s
230250K .......... .......... .......... .......... .......... 87% 25.9M 3s
230300K .......... .......... .......... .......... .......... 87% 13.7M 3s
230350K .......... .......... .......... .......... .......... 87% 15.1M 3s
230400K .......... .......... .......... .......... .......... 87% 15.1M 3s
230450K .......... .......... .......... .......... .......... 87% 10.2M 3s
230500K .......... .......... .......... .......... .......... 87% 13.1M 3s
230550K .......... .......... .......... .......... .......... 87% 11.5M 3s
230600K .......... .......... .......... .......... .......... 87% 8.05M 3s
230650K .......... .......... .......... .......... .......... 87% 9.28M 3s
230700K .......... .......... .......... .......... .......... 88% 12.4M 3s
230750K .......... .......... .......... .......... .......... 88% 12.2M 3s
230800K .......... .......... .......... .......... .......... 88% 8.75M 3s
230850K .......... .......... .......... .......... .......... 88% 7.57M 3s
230900K .......... .......... .......... .......... .......... 88% 7.53M 3s
230950K .......... .......... .......... .......... .......... 88% 6.18M 3s
231000K .......... .......... .......... .......... .......... 88% 15.1M 3s
231050K .......... .......... .......... .......... .......... 88% 14.1M 3s
231100K .......... .......... .......... .......... .......... 88% 13.9M 3s
231150K .......... .......... .......... .......... .......... 88% 16.7M 3s
231200K .......... .......... .......... .......... .......... 88% 16.6M 3s
231250K .......... .......... .......... .......... .......... 88% 18.9M 3s
231300K .......... .......... .......... .......... .......... 88% 18.9M 3s
231350K .......... .......... .......... .......... .......... 88% 17.1M 3s
231400K .......... .......... .......... .......... .......... 88% 15.5M 3s
231450K .......... .......... .......... .......... .......... 88% 7.79M 3s
231500K .......... .......... .......... .......... .......... 88% 10.8M 3s
231550K .......... .......... .......... .......... .......... 88% 7.29M 3s
231600K .......... .......... .......... .......... .......... 88% 6.32M 3s
231650K .......... .......... .......... .......... .......... 88% 10.6M 3s
231700K .......... .......... .......... .......... .......... 88% 11.5M 3s
231750K .......... .......... .......... .......... .......... 88% 9.05M 3s
231800K .......... .......... .......... .......... .......... 88% 16.8M 3s
231850K .......... .......... .......... .......... .......... 88% 9.92M 3s
231900K .......... .......... .......... .......... .......... 88% 12.0M 3s
231950K .......... .......... .......... .......... .......... 88% 11.1M 3s
232000K .......... .......... .......... .......... .......... 88% 9.69M 3s
232050K .......... .......... .......... .......... .......... 88% 15.2M 3s
232100K .......... .......... .......... .......... .......... 88% 18.5M 3s
232150K .......... .......... .......... .......... .......... 88% 19.8M 3s
232200K .......... .......... .......... .......... .......... 88% 18.0M 3s
232250K .......... .......... .......... .......... .......... 88% 19.3M 3s
232300K .......... .......... .......... .......... .......... 88% 23.3M 3s
232350K .......... .......... .......... .......... .......... 88% 18.6M 3s
232400K .......... .......... .......... .......... .......... 88% 18.2M 3s
232450K .......... .......... .......... .......... .......... 88% 11.6M 3s
232500K .......... .......... .......... .......... .......... 88% 18.0M 3s
232550K .......... .......... .......... .......... .......... 88% 14.5M 3s
232600K .......... .......... .......... .......... .......... 88% 12.6M 3s
232650K .......... .......... .......... .......... .......... 88% 10.8M 3s
232700K .......... .......... .......... .......... .......... 88% 6.26M 3s
232750K .......... .......... .......... .......... .......... 88% 9.77M 3s
232800K .......... .......... .......... .......... .......... 88% 11.8M 3s
232850K .......... .......... .......... .......... .......... 88% 8.70M 3s
232900K .......... .......... .......... .......... .......... 88% 12.5M 3s
232950K .......... .......... .......... .......... .......... 88% 10.1M 3s
233000K .......... .......... .......... .......... .......... 88% 14.2M 3s
233050K .......... .......... .......... .......... .......... 88% 11.1M 3s
233100K .......... .......... .......... .......... .......... 88% 8.63M 3s
233150K .......... .......... .......... .......... .......... 88% 14.0M 3s
233200K .......... .......... .......... .......... .......... 88% 14.1M 3s
233250K .......... .......... .......... .......... .......... 88% 13.5M 3s
233300K .......... .......... .......... .......... .......... 88% 13.9M 3s
233350K .......... .......... .......... .......... .......... 89% 14.5M 3s
233400K .......... .......... .......... .......... .......... 89% 14.7M 3s
233450K .......... .......... .......... .......... .......... 89% 17.7M 3s
233500K .......... .......... .......... .......... .......... 89% 15.7M 3s
233550K .......... .......... .......... .......... .......... 89% 18.8M 3s
233600K .......... .......... .......... .......... .......... 89% 14.6M 3s
233650K .......... .......... .......... .......... .......... 89% 13.3M 3s
233700K .......... .......... .......... .......... .......... 89% 9.47M 3s
233750K .......... .......... .......... .......... .......... 89% 12.7M 3s
233800K .......... .......... .......... .......... .......... 89% 7.28M 3s
233850K .......... .......... .......... .......... .......... 89% 5.39M 3s
233900K .......... .......... .......... .......... .......... 89% 8.77M 3s
233950K .......... .......... .......... .......... .......... 89% 6.52M 3s
234000K .......... .......... .......... .......... .......... 89% 7.43M 3s
234050K .......... .......... .......... .......... .......... 89% 9.63M 3s
234100K .......... .......... .......... .......... .......... 89% 7.40M 3s
234150K .......... .......... .......... .......... .......... 89% 6.63M 3s
234200K .......... .......... .......... .......... .......... 89% 4.55M 3s
234250K .......... .......... .......... .......... .......... 89% 5.62M 3s
234300K .......... .......... .......... .......... .......... 89% 7.51M 3s
234350K .......... .......... .......... .......... .......... 89% 6.74M 3s
234400K .......... .......... .......... .......... .......... 89% 7.26M 3s
234450K .......... .......... .......... .......... .......... 89% 7.03M 3s
234500K .......... .......... .......... .......... .......... 89% 8.40M 3s
234550K .......... .......... .......... .......... .......... 89% 9.93M 3s
234600K .......... .......... .......... .......... .......... 89% 11.6M 3s
234650K .......... .......... .......... .......... .......... 89% 14.4M 3s
234700K .......... .......... .......... .......... .......... 89% 9.07M 3s
234750K .......... .......... .......... .......... .......... 89% 11.7M 3s
234800K .......... .......... .......... .......... .......... 89% 14.6M 3s
234850K .......... .......... .......... .......... .......... 89% 14.3M 3s
234900K .......... .......... .......... .......... .......... 89% 19.7M 3s
234950K .......... .......... .......... .......... .......... 89% 19.6M 3s
235000K .......... .......... .......... .......... .......... 89% 18.8M 3s
235050K .......... .......... .......... .......... .......... 89% 24.0M 3s
235100K .......... .......... .......... .......... .......... 89% 23.8M 3s
235150K .......... .......... .......... .......... .......... 89% 33.7M 3s
235200K .......... .......... .......... .......... .......... 89% 26.1M 3s
235250K .......... .......... .......... .......... .......... 89% 18.9M 3s
235300K .......... .......... .......... .......... .......... 89% 34.7M 3s
235350K .......... .......... .......... .......... .......... 89% 11.9M 3s
235400K .......... .......... .......... .......... .......... 89% 17.3M 3s
235450K .......... .......... .......... .......... .......... 89% 11.5M 3s
235500K .......... .......... .......... .......... .......... 89% 12.9M 3s
235550K .......... .......... .......... .......... .......... 89% 14.4M 3s
235600K .......... .......... .......... .......... .......... 89% 9.73M 3s
235650K .......... .......... .......... .......... .......... 89% 7.19M 3s
235700K .......... .......... .......... .......... .......... 89% 5.01M 3s
235750K .......... .......... .......... .......... .......... 89% 11.9M 3s
235800K .......... .......... .......... .......... .......... 89% 10.3M 3s
235850K .......... .......... .......... .......... .......... 89% 8.36M 3s
235900K .......... .......... .......... .......... .......... 89% 8.00M 3s
235950K .......... .......... .......... .......... .......... 90% 6.97M 3s
236000K .......... .......... .......... .......... .......... 90% 5.22M 3s
236050K .......... .......... .......... .......... .......... 90% 6.05M 3s
236100K .......... .......... .......... .......... .......... 90% 8.27M 3s
236150K .......... .......... .......... .......... .......... 90% 8.92M 3s
236200K .......... .......... .......... .......... .......... 90% 11.6M 3s
236250K .......... .......... .......... .......... .......... 90% 19.0M 3s
236300K .......... .......... .......... .......... .......... 90% 19.4M 3s
236350K .......... .......... .......... .......... .......... 90% 14.3M 3s
236400K .......... .......... .......... .......... .......... 90% 20.2M 3s
236450K .......... .......... .......... .......... .......... 90% 20.5M 3s
236500K .......... .......... .......... .......... .......... 90% 19.5M 3s
236550K .......... .......... .......... .......... .......... 90% 15.2M 3s
236600K .......... .......... .......... .......... .......... 90% 17.5M 3s
236650K .......... .......... .......... .......... .......... 90% 11.1M 3s
236700K .......... .......... .......... .......... .......... 90% 6.73M 3s
236750K .......... .......... .......... .......... .......... 90% 10.6M 3s
236800K .......... .......... .......... .......... .......... 90% 10.4M 3s
236850K .......... .......... .......... .......... .......... 90% 7.23M 3s
236900K .......... .......... .......... .......... .......... 90% 9.51M 3s
236950K .......... .......... .......... .......... .......... 90% 9.21M 3s
237000K .......... .......... .......... .......... .......... 90% 9.21M 3s
237050K .......... .......... .......... .......... .......... 90% 9.74M 3s
237100K .......... .......... .......... .......... .......... 90% 8.57M 3s
237150K .......... .......... .......... .......... .......... 90% 11.0M 3s
237200K .......... .......... .......... .......... .......... 90% 17.5M 3s
237250K .......... .......... .......... .......... .......... 90% 14.6M 3s
237300K .......... .......... .......... .......... .......... 90% 10.9M 3s
237350K .......... .......... .......... .......... .......... 90% 1.82M 3s
237400K .......... .......... .......... .......... .......... 90% 9.06M 2s
237450K .......... .......... .......... .......... .......... 90% 11.4M 2s
237500K .......... .......... .......... .......... .......... 90% 15.5M 2s
237550K .......... .......... .......... .......... .......... 90% 19.2M 2s
237600K .......... .......... .......... .......... .......... 90% 17.3M 2s
237650K .......... .......... .......... .......... .......... 90% 15.9M 2s
237700K .......... .......... .......... .......... .......... 90% 14.7M 2s
237750K .......... .......... .......... .......... .......... 90% 15.3M 2s
237800K .......... .......... .......... .......... .......... 90% 22.4M 2s
237850K .......... .......... .......... .......... .......... 90% 22.5M 2s
237900K .......... .......... .......... .......... .......... 90% 24.3M 2s
237950K .......... .......... .......... .......... .......... 90% 19.2M 2s
238000K .......... .......... .......... .......... .......... 90% 22.2M 2s
238050K .......... .......... .......... .......... .......... 90% 26.8M 2s
238100K .......... .......... .......... .......... .......... 90% 12.0M 2s
238150K .......... .......... .......... .......... .......... 90% 9.28M 2s
238200K .......... .......... .......... .......... .......... 90% 8.62M 2s
238250K .......... .......... .......... .......... .......... 90% 9.52M 2s
238300K .......... .......... .......... .......... .......... 90% 12.9M 2s
238350K .......... .......... .......... .......... .......... 90% 11.9M 2s
238400K .......... .......... .......... .......... .......... 90% 7.93M 2s
238450K .......... .......... .......... .......... .......... 90% 6.37M 2s
238500K .......... .......... .......... .......... .......... 90% 7.63M 2s
238550K .......... .......... .......... .......... .......... 91% 6.50M 2s
238600K .......... .......... .......... .......... .......... 91% 7.29M 2s
238650K .......... .......... .......... .......... .......... 91% 18.3M 2s
238700K .......... .......... .......... .......... .......... 91% 14.7M 2s
238750K .......... .......... .......... .......... .......... 91% 17.4M 2s
238800K .......... .......... .......... .......... .......... 91% 16.1M 2s
238850K .......... .......... .......... .......... .......... 91% 16.1M 2s
238900K .......... .......... .......... .......... .......... 91% 16.2M 2s
238950K .......... .......... .......... .......... .......... 91% 19.2M 2s
239000K .......... .......... .......... .......... .......... 91% 10.9M 2s
239050K .......... .......... .......... .......... .......... 91% 10.2M 2s
239100K .......... .......... .......... .......... .......... 91% 12.1M 2s
239150K .......... .......... .......... .......... .......... 91% 19.2M 2s
239200K .......... .......... .......... .......... .......... 91% 12.8M 2s
239250K .......... .......... .......... .......... .......... 91% 21.0M 2s
239300K .......... .......... .......... .......... .......... 91% 12.2M 2s
239350K .......... .......... .......... .......... .......... 91% 13.9M 2s
239400K .......... .......... .......... .......... .......... 91% 18.9M 2s
239450K .......... .......... .......... .......... .......... 91% 15.4M 2s
239500K .......... .......... .......... .......... .......... 91% 10.4M 2s
239550K .......... .......... .......... .......... .......... 91% 10.5M 2s
239600K .......... .......... .......... .......... .......... 91% 7.49M 2s
239650K .......... .......... .......... .......... .......... 91% 10.5M 2s
239700K .......... .......... .......... .......... .......... 91% 14.0M 2s
239750K .......... .......... .......... .......... .......... 91% 15.0M 2s
239800K .......... .......... .......... .......... .......... 91% 11.8M 2s
239850K .......... .......... .......... .......... .......... 91% 6.97M 2s
239900K .......... .......... .......... .......... .......... 91% 16.1M 2s
239950K .......... .......... .......... .......... .......... 91% 9.16M 2s
240000K .......... .......... .......... .......... .......... 91% 9.44M 2s
240050K .......... .......... .......... .......... .......... 91% 9.40M 2s
240100K .......... .......... .......... .......... .......... 91% 9.97M 2s
240150K .......... .......... .......... .......... .......... 91% 21.5M 2s
240200K .......... .......... .......... .......... .......... 91% 12.7M 2s
240250K .......... .......... .......... .......... .......... 91% 11.0M 2s
240300K .......... .......... .......... .......... .......... 91% 14.9M 2s
240350K .......... .......... .......... .......... .......... 91% 7.08M 2s
240400K .......... .......... .......... .......... .......... 91% 8.08M 2s
240450K .......... .......... .......... .......... .......... 91% 8.84M 2s
240500K .......... .......... .......... .......... .......... 91% 10.1M 2s
240550K .......... .......... .......... .......... .......... 91% 12.1M 2s
240600K .......... .......... .......... .......... .......... 91% 9.98M 2s
240650K .......... .......... .......... .......... .......... 91% 13.4M 2s
240700K .......... .......... .......... .......... .......... 91% 10.9M 2s
240750K .......... .......... .......... .......... .......... 91% 22.4M 2s
240800K .......... .......... .......... .......... .......... 91% 14.4M 2s
240850K .......... .......... .......... .......... .......... 91% 22.3M 2s
240900K .......... .......... .......... .......... .......... 91% 23.3M 2s
240950K .......... .......... .......... .......... .......... 91% 26.7M 2s
241000K .......... .......... .......... .......... .......... 91% 38.3M 2s
241050K .......... .......... .......... .......... .......... 91% 28.7M 2s
241100K .......... .......... .......... .......... .......... 91% 27.4M 2s
241150K .......... .......... .......... .......... .......... 91% 15.6M 2s
241200K .......... .......... .......... .......... .......... 92% 11.6M 2s
241250K .......... .......... .......... .......... .......... 92% 11.4M 2s
241300K .......... .......... .......... .......... .......... 92% 12.1M 2s
241350K .......... .......... .......... .......... .......... 92% 10.0M 2s
241400K .......... .......... .......... .......... .......... 92% 8.74M 2s
241450K .......... .......... .......... .......... .......... 92% 8.96M 2s
241500K .......... .......... .......... .......... .......... 92% 9.05M 2s
241550K .......... .......... .......... .......... .......... 92% 8.65M 2s
241600K .......... .......... .......... .......... .......... 92% 5.71M 2s
241650K .......... .......... .......... .......... .......... 92% 5.64M 2s
241700K .......... .......... .......... .......... .......... 92% 7.30M 2s
241750K .......... .......... .......... .......... .......... 92% 10.7M 2s
241800K .......... .......... .......... .......... .......... 92% 9.01M 2s
241850K .......... .......... .......... .......... .......... 92% 9.16M 2s
241900K .......... .......... .......... .......... .......... 92% 10.8M 2s
241950K .......... .......... .......... .......... .......... 92% 6.73M 2s
242000K .......... .......... .......... .......... .......... 92% 9.14M 2s
242050K .......... .......... .......... .......... .......... 92% 10.1M 2s
242100K .......... .......... .......... .......... .......... 92% 9.11M 2s
242150K .......... .......... .......... .......... .......... 92% 11.0M 2s
242200K .......... .......... .......... .......... .......... 92% 10.0M 2s
242250K .......... .......... .......... .......... .......... 92% 11.7M 2s
242300K .......... .......... .......... .......... .......... 92% 10.9M 2s
242350K .......... .......... .......... .......... .......... 92% 11.2M 2s
242400K .......... .......... .......... .......... .......... 92% 12.4M 2s
242450K .......... .......... .......... .......... .......... 92% 11.1M 2s
242500K .......... .......... .......... .......... .......... 92% 15.0M 2s
242550K .......... .......... .......... .......... .......... 92% 8.77M 2s
242600K .......... .......... .......... .......... .......... 92% 7.95M 2s
242650K .......... .......... .......... .......... .......... 92% 19.8M 2s
242700K .......... .......... .......... .......... .......... 92% 14.7M 2s
242750K .......... .......... .......... .......... .......... 92% 20.7M 2s
242800K .......... .......... .......... .......... .......... 92% 21.9M 2s
242850K .......... .......... .......... .......... .......... 92% 10.2M 2s
242900K .......... .......... .......... .......... .......... 92% 14.6M 2s
242950K .......... .......... .......... .......... .......... 92% 12.2M 2s
243000K .......... .......... .......... .......... .......... 92% 12.9M 2s
243050K .......... .......... .......... .......... .......... 92% 11.5M 2s
243100K .......... .......... .......... .......... .......... 92% 6.85M 2s
243150K .......... .......... .......... .......... .......... 92% 4.94M 2s
243200K .......... .......... .......... .......... .......... 92% 6.35M 2s
243250K .......... .......... .......... .......... .......... 92% 8.16M 2s
243300K .......... .......... .......... .......... .......... 92% 13.3M 2s
243350K .......... .......... .......... .......... .......... 92% 6.96M 2s
243400K .......... .......... .......... .......... .......... 92% 11.6M 2s
243450K .......... .......... .......... .......... .......... 92% 14.5M 2s
243500K .......... .......... .......... .......... .......... 92% 20.1M 2s
243550K .......... .......... .......... .......... .......... 92% 15.4M 2s
243600K .......... .......... .......... .......... .......... 92% 16.0M 2s
243650K .......... .......... .......... .......... .......... 92% 25.2M 2s
243700K .......... .......... .......... .......... .......... 92% 9.95M 2s
243750K .......... .......... .......... .......... .......... 92% 11.4M 2s
243800K .......... .......... .......... .......... .......... 93% 8.14M 2s
243850K .......... .......... .......... .......... .......... 93% 9.10M 2s
243900K .......... .......... .......... .......... .......... 93% 12.2M 2s
243950K .......... .......... .......... .......... .......... 93% 7.50M 2s
244000K .......... .......... .......... .......... .......... 93% 10.7M 2s
244050K .......... .......... .......... .......... .......... 93% 12.2M 2s
244100K .......... .......... .......... .......... .......... 93% 7.64M 2s
244150K .......... .......... .......... .......... .......... 93% 11.0M 2s
244200K .......... .......... .......... .......... .......... 93% 8.21M 2s
244250K .......... .......... .......... .......... .......... 93% 9.69M 2s
244300K .......... .......... .......... .......... .......... 93% 8.48M 2s
244350K .......... .......... .......... .......... .......... 93% 6.64M 2s
244400K .......... .......... .......... .......... .......... 93% 9.31M 2s
244450K .......... .......... .......... .......... .......... 93% 7.86M 2s
244500K .......... .......... .......... .......... .......... 93% 8.63M 2s
244550K .......... .......... .......... .......... .......... 93% 5.24M 2s
244600K .......... .......... .......... .......... .......... 93% 4.08M 2s
244650K .......... .......... .......... .......... .......... 93% 1.82M 2s
244700K .......... .......... .......... .......... .......... 93% 3.01M 2s
244750K .......... .......... .......... .......... .......... 93% 3.39M 2s
244800K .......... .......... .......... .......... .......... 93% 2.98M 2s
244850K .......... .......... .......... .......... .......... 93% 2.76M 2s
244900K .......... .......... .......... .......... .......... 93% 4.12M 2s
244950K .......... .......... .......... .......... .......... 93% 1.89M 2s
245000K .......... .......... .......... .......... .......... 93% 1019K 2s
245050K .......... .......... .......... .......... .......... 93% 4.24M 2s
245100K .......... .......... .......... .......... .......... 93% 3.65M 2s
245150K .......... .......... .......... .......... .......... 93% 6.29M 2s
245200K .......... .......... .......... .......... .......... 93% 13.7M 2s
245250K .......... .......... .......... .......... .......... 93% 42.4M 2s
245300K .......... .......... .......... .......... .......... 93% 19.6M 2s
245350K .......... .......... .......... .......... .......... 93% 22.0M 2s
245400K .......... .......... .......... .......... .......... 93% 17.0M 2s
245450K .......... .......... .......... .......... .......... 93% 11.5M 2s
245500K .......... .......... .......... .......... .......... 93% 13.7M 2s
245550K .......... .......... .......... .......... .......... 93% 11.9M 2s
245600K .......... .......... .......... .......... .......... 93% 11.4M 2s
245650K .......... .......... .......... .......... .......... 93% 10.0M 2s
245700K .......... .......... .......... .......... .......... 93% 9.24M 2s
245750K .......... .......... .......... .......... .......... 93% 10.3M 2s
245800K .......... .......... .......... .......... .......... 93% 18.8M 2s
245850K .......... .......... .......... .......... .......... 93% 20.2M 2s
245900K .......... .......... .......... .......... .......... 93% 15.0M 2s
245950K .......... .......... .......... .......... .......... 93% 22.1M 2s
246000K .......... .......... .......... .......... .......... 93% 18.9M 2s
246050K .......... .......... .......... .......... .......... 93% 15.2M 2s
246100K .......... .......... .......... .......... .......... 93% 24.3M 2s
246150K .......... .......... .......... .......... .......... 93% 32.0M 2s
246200K .......... .......... .......... .......... .......... 93% 13.8M 2s
246250K .......... .......... .......... .......... .......... 93% 20.3M 2s
246300K .......... .......... .......... .......... .......... 93% 18.8M 2s
246350K .......... .......... .......... .......... .......... 93% 9.26M 2s
246400K .......... .......... .......... .......... .......... 93% 14.2M 2s
246450K .......... .......... .......... .......... .......... 94% 18.6M 2s
246500K .......... .......... .......... .......... .......... 94% 12.8M 2s
246550K .......... .......... .......... .......... .......... 94% 20.0M 2s
246600K .......... .......... .......... .......... .......... 94% 11.6M 2s
246650K .......... .......... .......... .......... .......... 94% 12.1M 2s
246700K .......... .......... .......... .......... .......... 94% 16.7M 2s
246750K .......... .......... .......... .......... .......... 94% 13.0M 2s
246800K .......... .......... .......... .......... .......... 94% 20.2M 2s
246850K .......... .......... .......... .......... .......... 94% 15.0M 2s
246900K .......... .......... .......... .......... .......... 94% 22.6M 2s
246950K .......... .......... .......... .......... .......... 94% 14.2M 2s
247000K .......... .......... .......... .......... .......... 94% 20.3M 2s
247050K .......... .......... .......... .......... .......... 94% 15.0M 2s
247100K .......... .......... .......... .......... .......... 94% 12.6M 2s
247150K .......... .......... .......... .......... .......... 94% 16.1M 2s
247200K .......... .......... .......... .......... .......... 94% 11.4M 2s
247250K .......... .......... .......... .......... .......... 94% 11.2M 2s
247300K .......... .......... .......... .......... .......... 94% 10.1M 1s
247350K .......... .......... .......... .......... .......... 94% 19.8M 1s
247400K .......... .......... .......... .......... .......... 94% 24.8M 1s
247450K .......... .......... .......... .......... .......... 94% 20.2M 1s
247500K .......... .......... .......... .......... .......... 94% 20.8M 1s
247550K .......... .......... .......... .......... .......... 94% 19.2M 1s
247600K .......... .......... .......... .......... .......... 94% 12.2M 1s
247650K .......... .......... .......... .......... .......... 94% 19.1M 1s
247700K .......... .......... .......... .......... .......... 94% 11.1M 1s
247750K .......... .......... .......... .......... .......... 94% 13.0M 1s
247800K .......... .......... .......... .......... .......... 94% 11.4M 1s
247850K .......... .......... .......... .......... .......... 94% 9.69M 1s
247900K .......... .......... .......... .......... .......... 94% 8.27M 1s
247950K .......... .......... .......... .......... .......... 94% 12.1M 1s
248000K .......... .......... .......... .......... .......... 94% 17.4M 1s
248050K .......... .......... .......... .......... .......... 94% 17.3M 1s
248100K .......... .......... .......... .......... .......... 94% 11.8M 1s
248150K .......... .......... .......... .......... .......... 94% 11.1M 1s
248200K .......... .......... .......... .......... .......... 94% 11.1M 1s
248250K .......... .......... .......... .......... .......... 94% 11.9M 1s
248300K .......... .......... .......... .......... .......... 94% 11.8M 1s
248350K .......... .......... .......... .......... .......... 94% 9.33M 1s
248400K .......... .......... .......... .......... .......... 94% 15.1M 1s
248450K .......... .......... .......... .......... .......... 94% 7.43M 1s
248500K .......... .......... .......... .......... .......... 94% 11.4M 1s
248550K .......... .......... .......... .......... .......... 94% 11.2M 1s
248600K .......... .......... .......... .......... .......... 94% 7.01M 1s
248650K .......... .......... .......... .......... .......... 94% 15.3M 1s
248700K .......... .......... .......... .......... .......... 94% 11.4M 1s
248750K .......... .......... .......... .......... .......... 94% 16.3M 1s
248800K .......... .......... .......... .......... .......... 94% 12.8M 1s
248850K .......... .......... .......... .......... .......... 94% 10.3M 1s
248900K .......... .......... .......... .......... .......... 94% 11.1M 1s
248950K .......... .......... .......... .......... .......... 94% 7.11M 1s
249000K .......... .......... .......... .......... .......... 94% 9.22M 1s
249050K .......... .......... .......... .......... .......... 95% 9.30M 1s
249100K .......... .......... .......... .......... .......... 95% 8.44M 1s
249150K .......... .......... .......... .......... .......... 95% 12.9M 1s
249200K .......... .......... .......... .......... .......... 95% 13.3M 1s
249250K .......... .......... .......... .......... .......... 95% 14.0M 1s
249300K .......... .......... .......... .......... .......... 95% 15.4M 1s
249350K .......... .......... .......... .......... .......... 95% 9.16M 1s
249400K .......... .......... .......... .......... .......... 95% 12.7M 1s
249450K .......... .......... .......... .......... .......... 95% 7.47M 1s
249500K .......... .......... .......... .......... .......... 95% 10.4M 1s
249550K .......... .......... .......... .......... .......... 95% 8.23M 1s
249600K .......... .......... .......... .......... .......... 95% 7.13M 1s
249650K .......... .......... .......... .......... .......... 95% 8.72M 1s
249700K .......... .......... .......... .......... .......... 95% 7.18M 1s
249750K .......... .......... .......... .......... .......... 95% 11.9M 1s
249800K .......... .......... .......... .......... .......... 95% 9.08M 1s
249850K .......... .......... .......... .......... .......... 95% 8.57M 1s
249900K .......... .......... .......... .......... .......... 95% 20.8M 1s
249950K .......... .......... .......... .......... .......... 95% 9.85M 1s
250000K .......... .......... .......... .......... .......... 95% 9.28M 1s
250050K .......... .......... .......... .......... .......... 95% 13.0M 1s
250100K .......... .......... .......... .......... .......... 95% 8.57M 1s
250150K .......... .......... .......... .......... .......... 95% 9.26M 1s
250200K .......... .......... .......... .......... .......... 95% 5.85M 1s
250250K .......... .......... .......... .......... .......... 95% 6.56M 1s
250300K .......... .......... .......... .......... .......... 95% 5.16M 1s
250350K .......... .......... .......... .......... .......... 95% 4.92M 1s
250400K .......... .......... .......... .......... .......... 95% 6.74M 1s
250450K .......... .......... .......... .......... .......... 95% 7.87M 1s
250500K .......... .......... .......... .......... .......... 95% 9.56M 1s
250550K .......... .......... .......... .......... .......... 95% 9.53M 1s
250600K .......... .......... .......... .......... .......... 95% 15.1M 1s
250650K .......... .......... .......... .......... .......... 95% 20.2M 1s
250700K .......... .......... .......... .......... .......... 95% 16.5M 1s
250750K .......... .......... .......... .......... .......... 95% 19.1M 1s
250800K .......... .......... .......... .......... .......... 95% 19.9M 1s
250850K .......... .......... .......... .......... .......... 95% 14.9M 1s
250900K .......... .......... .......... .......... .......... 95% 15.2M 1s
250950K .......... .......... .......... .......... .......... 95% 15.9M 1s
251000K .......... .......... .......... .......... .......... 95% 20.3M 1s
251050K .......... .......... .......... .......... .......... 95% 12.6M 1s
251100K .......... .......... .......... .......... .......... 95% 23.5M 1s
251150K .......... .......... .......... .......... .......... 95% 15.1M 1s
251200K .......... .......... .......... .......... .......... 95% 14.7M 1s
251250K .......... .......... .......... .......... .......... 95% 12.0M 1s
251300K .......... .......... .......... .......... .......... 95% 11.3M 1s
251350K .......... .......... .......... .......... .......... 95% 7.57M 1s
251400K .......... .......... .......... .......... .......... 95% 11.1M 1s
251450K .......... .......... .......... .......... .......... 95% 5.89M 1s
251500K .......... .......... .......... .......... .......... 95%  881K 1s
251550K .......... .......... .......... .......... .......... 95% 10.8M 1s
251600K .......... .......... .......... .......... .......... 95% 9.95M 1s
251650K .......... .......... .......... .......... .......... 95% 13.6M 1s
251700K .......... .......... .......... .......... .......... 96% 11.2M 1s
251750K .......... .......... .......... .......... .......... 96% 13.2M 1s
251800K .......... .......... .......... .......... .......... 96% 12.3M 1s
251850K .......... .......... .......... .......... .......... 96% 11.8M 1s
251900K .......... .......... .......... .......... .......... 96% 12.8M 1s
251950K .......... .......... .......... .......... .......... 96% 14.8M 1s
252000K .......... .......... .......... .......... .......... 96% 31.1M 1s
252050K .......... .......... .......... .......... .......... 96% 23.4M 1s
252100K .......... .......... .......... .......... .......... 96% 13.8M 1s
252150K .......... .......... .......... .......... .......... 96% 14.2M 1s
252200K .......... .......... .......... .......... .......... 96% 10.1M 1s
252250K .......... .......... .......... .......... .......... 96% 2.45M 1s
252300K .......... .......... .......... .......... .......... 96% 4.59M 1s
252350K .......... .......... .......... .......... .......... 96% 5.33M 1s
252400K .......... .......... .......... .......... .......... 96% 14.7M 1s
252450K .......... .......... .......... .......... .......... 96% 9.11M 1s
252500K .......... .......... .......... .......... .......... 96% 9.11M 1s
252550K .......... .......... .......... .......... .......... 96% 10.6M 1s
252600K .......... .......... .......... .......... .......... 96% 7.11M 1s
252650K .......... .......... .......... .......... .......... 96% 14.4M 1s
252700K .......... .......... .......... .......... .......... 96% 11.0M 1s
252750K .......... .......... .......... .......... .......... 96% 8.85M 1s
252800K .......... .......... .......... .......... .......... 96% 8.73M 1s
252850K .......... .......... .......... .......... .......... 96% 12.9M 1s
252900K .......... .......... .......... .......... .......... 96% 14.5M 1s
252950K .......... .......... .......... .......... .......... 96% 16.2M 1s
253000K .......... .......... .......... .......... .......... 96% 13.9M 1s
253050K .......... .......... .......... .......... .......... 96% 12.0M 1s
253100K .......... .......... .......... .......... .......... 96% 22.6M 1s
253150K .......... .......... .......... .......... .......... 96% 16.9M 1s
253200K .......... .......... .......... .......... .......... 96% 11.7M 1s
253250K .......... .......... .......... .......... .......... 96% 16.5M 1s
253300K .......... .......... .......... .......... .......... 96% 17.6M 1s
253350K .......... .......... .......... .......... .......... 96% 14.3M 1s
253400K .......... .......... .......... .......... .......... 96% 16.6M 1s
253450K .......... .......... .......... .......... .......... 96% 16.8M 1s
253500K .......... .......... .......... .......... .......... 96% 17.3M 1s
253550K .......... .......... .......... .......... .......... 96% 18.3M 1s
253600K .......... .......... .......... .......... .......... 96% 18.7M 1s
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2024-04-27 17:49:08 (9.83 MB/s) - ‘ESPbeta.tgz’ saved [268487989/268487989]

+ 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/7.7/LINUX64/EngSketchPad/config/
+ ./makeEnv

ESP runtime AutoConfigurator

CASROOT = /home/jenkins/util/ESP/OpenCASCADE-7.7.0  with contents:
bin
include
lib
share


Info: Python exec /home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad
EFCOMP   = gfortran

CARCH    = LINUX64
CASROOT  = /home/jenkins/util/ESP/OpenCASCADE-7.7.0
CASARCH  = .
CASREV   = 7.7

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/7.7/LINUX64/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=LINUX64
++ ESP_ARCH=LINUX64
++ export ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad
++ ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad
++ export CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.7.0
++ CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.7.0
++ export CASARCH=.
++ CASARCH=.
++ export CASREV=7.7
++ CASREV=7.7
++ export PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.7/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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.7/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:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/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/7.7/LINUX64/EngSketchPad/pyESP:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9//lib: ']'
++ export LD_LIBRARY_PATH=/home/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9//lib:
++ LD_LIBRARY_PATH=/home/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9//lib:
++ export UDUNITS2_XML_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ export CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/SLUGS/Slugs.html &'
++ SLUGS_START='firefox /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/SLUGS/Slugs.html &'
++ export 'ESP_START=firefox /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/ESP/ESP.html &'
++ ESP_START='firefox /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/ESP/ESP.html &'
++ export 'WV_START=firefox /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/wvClient/wv.html &'
++ WV_START='firefox /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/wvClient/wv.html &'
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src
+ make
(cd EGADS/src; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/src'
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/LINUX64
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/LINUX64
cp -p ../include/LINUX64 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/LINUX64
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/STANALYZER.make
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/STANALYZER.make
cp -p ../include/STANALYZER.make /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/STANALYZER.make
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads.h
cp -p ../include/egads.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads_dot.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads_dot.h
cp -p ../include/egads_dot.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads_dot.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads.inc
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads.inc
cp -p ../include/egads.inc /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads.inc
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsErrors.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsErrors.h
cp -p ../include/egadsErrors.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsErrors.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsTypes.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsTypes.h
cp -p ../include/egadsTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsTypes.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/emp.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/emp.h
cp -p ../include/emp.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/emp.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/prm.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/prm.h
cp -p ../include/prm.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/prm.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsserver.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsserver.h
cp -p ../include/wsserver.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsserver.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsserver.inc
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsserver.inc
cp -p ../include/wsserver.inc /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsserver.inc
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsss.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsss.h
cp -p ../include/wsss.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsss.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsTris.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsTris.h
cp -p egadsTris.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsTris.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsSplineFit.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsSplineFit.h
cp -p egadsSplineFit.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsSplineFit.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsSplineVels.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsSplineVels.h
cp -p egadsSplineVels.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsSplineVels.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsf90.inc
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsf90.inc
cp -p ../include/egadsf90.inc /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsf90.inc
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal/SurrealD.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Lazy.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal/SurrealD_Lazy.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Trad.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal/SurrealD_Trad.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal/SurrealS.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Lazy.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal/SurrealS_Lazy.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Trad.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal/SurrealS_Trad.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/always_inline.h /home/jenkins/workspace/ESP_Beta/7.7/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=7.7  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include 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=7.7  -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=7.7  -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=7.7  -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=7.7  -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=7.7  -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=7.7  -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=7.7  -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=7.7  -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=7.7  -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=7.7  -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=7.7  -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=7.7  -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=7.7  -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=7.7  -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=7.7  -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=7.7  -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=7.7 -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=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7 -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7 -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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/7.7/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=7.7 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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 egadsUVmap.c -Iuvmap \
	-o ./egadsUVmap.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libuvmap.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libuvmap.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/lib/libuvmap.a
gcc -g  -o ./uvmap.exe ./uvmap.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -luvmap -lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/util'
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegads.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegads.so
(cd .; gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/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-7.7.0/./lib -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet -pthread -lm -lstdc++ -lrt )
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadstatic.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadstatic.a
cp /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libuvmap.a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadstatic.a
(cd .; \
	ar rs /home/jenkins/workspace/ESP_Beta/7.7/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=7.7  -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=7.7  -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=7.7  -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=7.7  -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=7.7  -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=7.7  -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=7.7  -I../include fgadsTopo.c -o ./fgadsTopo.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libfgads.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libfgads.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/lib/libfgads.a
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libemp.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libemp.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libemp.a emp.o;  )
ar: creating /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libemp.a
 *** EGADS Build Complete! ***
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/src'
(cd EGADS/lite; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 ../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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -DLITE -I../include -I. -I../src \
                -I../util/uvmap liteUVmap.c -o ./liteUVmap.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadslite.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadslite.so
(cd .; gcc -g  -shared -Wl,-no-undefined \
	-o /home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/lib/libegadslitestatic.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadslitestatic.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/lib/libegadslitestatic.a
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/lite'
(cd wvServer; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/LINUX64/EngSketchPad/include fwv.c -o ./fwv.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libwsserver.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libwsserver.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.7/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/7.7/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/7.7/LINUX64/EngSketchPad/include -I. -o ./servertest.o
g++ -g  -o ./server ./servertest.o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libwsserver.a  \
	-lpthread -lz -lm
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libwsserver.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libwsserver.so
(cd .; g++ -g  -shared -Wl,-no-undefined \
	-o /home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/wvServer'
(cd EGADS/examples; make -f egads2cart.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include egads2cart.c \
	-o ./egads2cart.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/egads2cart ./egads2cart.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -legads \
	-lrt -lm
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vCurvature.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include vCurvature.c -o ./vCurvature.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/vCurvature ./vCurvature.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lwsserver -legads -lrt
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vGeom.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include vGeom.c -o ./vGeom.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/vGeom ./vGeom.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lwsserver -legads \
	-lrt
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vTess.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include ../util/retessFaces.c \
	-o ./retessFaces.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/vTesstatic ./vTess.o ./retessFaces.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lwsserver -legadstatic -L/home/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet -pthread -lm \
	-lpthread -lz -lrt -lm
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/vTess ./vTess.o ./retessFaces.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lwsserver -legads -lrt
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/examples'
(cd OpenCSM; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. tim.c -o ./tim.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libocsm.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libocsm.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libocsm.so ./OpenCSM.o ./udp.o ./tim.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -legads -lwsserver -ldl -lrt -lm
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/serveCSM ./serveCSM.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. serveESP.c -o ./serveESP.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/serveESP ./serveESP.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. sensCSM.c -o ./sensCSM.o
gcc -g  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/sensCSM ./sensCSM.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpBezier.c -o ./udpBezier.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bezier.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bezier.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bezier.so ./udpBezier.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpBiconvex.c -o ./udpBiconvex.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/biconvex.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/biconvex.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/biconvex.so ./udpBiconvex.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpBox.c -o ./udpBox.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/box.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/box.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/box.so ./udpBox.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpBspline.c -o ./udpBspline.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bspline.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bspline.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bspline.so ./udpBspline.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfCatmull.c -o ./udfCatmull.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/catmull.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/catmull.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/catmull.so ./udfCatmull.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfCompare.c -o ./udfCompare.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/compare.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/compare.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/compare.so ./udfCompare.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfCreateBEM.c -o ./udfCreateBEM.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/createBEM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/createBEM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/createBEM.so ./udfCreateBEM.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfCreatePoly.c -o ./udfCreatePoly.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/createPoly.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/createPoly.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/createPoly.so ./udfCreatePoly.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpCsm.c -o ./udpCsm.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/csm.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/csm.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/csm.so ./udpCsm.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfDeform.c -o ./udfDeform.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/deform.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/deform.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/deform.so ./udfDeform.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfDroop.c -o ./udfDroop.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/droop.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/droop.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/droop.so ./udfDroop.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfDumpPmtrs.c -o ./udfDumpPmtrs.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/dumpPmtrs.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/dumpPmtrs.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/dumpPmtrs.so ./udfDumpPmtrs.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfEditAttr.c -o ./udfEditAttr.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/editAttr.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/editAttr.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/editAttr.so ./udfEditAttr.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpEllipse.c -o ./udpEllipse.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ellipse.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ellipse.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ellipse.so ./udpEllipse.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpEqn2body.c -o ./udpEqn2body.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/eqn2body.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/eqn2body.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/eqn2body.so ./udpEqn2body.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpFitcurve.c -o ./udpFitcurve.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/fitcurve.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/fitcurve.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/fitcurve.so ./udpFitcurve.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfFlend.c -o ./udfFlend.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/flend.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/flend.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/flend.so ./udfFlend.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpFreeform.c -o ./udpFreeform.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/freeform.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/freeform.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/freeform.so ./udpFreeform.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfGanged.c -o ./udfGanged.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ganged.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ganged.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ganged.so ./udfGanged.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfGuide.c -o ./udfGuide.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/guide.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/guide.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/guide.so ./udfGuide.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpHex.c -o ./udpHex.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/hex.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/hex.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/hex.so ./udpHex.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpImport.c -o ./udpImport.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/import.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/import.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/import.so ./udpImport.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpKulfan.c -o ./udpKulfan.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/kulfan.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/kulfan.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/kulfan.so ./udpKulfan.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfLinalg.c -o ./udfLinalg.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/linalg.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/linalg.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/linalg.so ./udfLinalg.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfMatchBodys.c -o ./udfMatchBodys.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/matchBodys.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/matchBodys.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/matchBodys.so ./udfMatchBodys.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfMechanism.c -o ./udfMechanism.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mechanism.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mechanism.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mechanism.so ./udfMechanism.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpNaca.c -o ./udpNaca.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca.so ./udpNaca.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfNaca6mc.c -o ./udfNaca6mc.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca6mc.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca6mc.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca6mc.so ./udfNaca6mc.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfNacelle.c -o ./udfNacelle.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nacelle.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nacelle.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nacelle.so ./udfNacelle.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpNurbbody.c -o ./udpNurbbody.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nurbbody.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nurbbody.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nurbbody.so ./udpNurbbody.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfNuscale.c -o ./udfNuscale.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nuscale.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nuscale.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nuscale.so ./udfNuscale.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfOffset.c -o ./udfOffset.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/offset.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/offset.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/offset.so ./udfOffset.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpParabaloid.c -o ./udpParabaloid.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/parabaloid.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/parabaloid.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/parabaloid.so ./udpParabaloid.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpParsec.cpp -o ./udpParsec.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/parsec.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/parsec.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/parsec.so ./udpParsec.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpPod.c -o ./udpPod.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pod.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pod.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pod.so ./udpPod.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpPoly.c -o ./udpPoly.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/poly.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/poly.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/poly.so ./udpPoly.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfPrintBbox.c -o ./udfPrintBbox.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printBbox.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printBbox.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printBbox.so ./udfPrintBbox.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfPrintBrep.c -o ./udfPrintBrep.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printBrep.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printBrep.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printBrep.so ./udfPrintBrep.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfPrintEgo.c -o ./udfPrintEgo.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printEgo.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printEgo.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printEgo.so ./udfPrintEgo.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpProp.c -o ./udpProp.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/prop.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/prop.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/prop.so ./udpProp.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpRadwaf.c -o ./udpRadwaf.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/radwaf.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/radwaf.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/radwaf.so ./udpRadwaf.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpSample.c -o ./udpSample.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/sample.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/sample.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/sample.so ./udpSample.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpSew.c -o ./udpSew.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/sew.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/sew.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/sew.so ./udpSew.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfShadow.c -o ./udfShadow.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/shadow.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/shadow.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/shadow.so ./udfShadow.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfSlices.c -o ./udfSlices.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/slices.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/slices.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/slices.so ./udfSlices.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpStag.c -o ./udpStag.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stag.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stag.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stag.so ./udpStag.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfStiffener.c -o ./udfStiffener.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stiffener.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stiffener.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stiffener.so ./udfStiffener.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpSupell.c -o ./udpSupell.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/supell.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/supell.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/supell.so ./udpSupell.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfTester1.c -o ./udfTester1.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tester1.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tester1.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tester1.so ./udfTester1.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpTester2.c -o ./udpTester2.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tester2.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tester2.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tester2.so ./udpTester2.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpVsp3.c -o ./udpVsp3.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vsp3.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vsp3.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vsp3.so ./udpVsp3.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpWaffle.c -o ./udpWaffle.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/waffle.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/waffle.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/waffle.so ./udpWaffle.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpWarp.c -o ./udpWarp.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/warp.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/warp.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/warp.so ./udpWarp.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. eggPDT2.c -o ./eggPDT2.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/PDT2.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/PDT2.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/PDT2.so ./eggPDT2.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/lib/naca456.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca456.so
gfortran -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca456.so ./udpNaca456.o ./naca456.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timEreped.c -o ./timEreped.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ereped.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ereped.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ereped.so ./timEreped.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timMitten.c -o ./timMitten.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mitten.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mitten.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mitten.so ./timMitten.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timPlotter.c -o ./timPlotter.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/plotter.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/plotter.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/plotter.so ./timPlotter.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timPlugs.c -o ./timPlugs.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/plugs.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/plugs.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/plugs.so ./timPlugs.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timSlugs.c -o ./timSlugs.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/slugs.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/slugs.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/slugs.so ./timSlugs.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timVspSetup.c -o ./timVspSetup.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vspSetup.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vspSetup.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vspSetup.so ./timVspSetup.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/OpenCSM.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/OpenCSM.h
cp -p OpenCSM.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/OpenCSM.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/common.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/common.h
cp -p common.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/common.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udp.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udp.h
cp -p udp.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udp.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/esp.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/esp.h
cp -p esp.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/esp.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/tim.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/tim.h
cp -p tim.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/tim.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egg.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egg.h
cp -p egg.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egg.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udpUtilities.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udpUtilities.h
cp -p udpUtilities.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udpUtilities.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udpUtilities.c
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udpUtilities.c
cp -p udpUtilities.c /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udpUtilities.c
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/OpenCSM'
(cd Slugs; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. Tessellate.c \
	-o ./Tessellate.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/Slugs ./Slugs.o ./Fitter.o ./RedBlackTree.o \
	./Tessellate.o -lrt -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. TestFit.c -o ./TestFit.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/TestFit ./TestFit.o ./Fitter.o -lrt -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -legads \
	-lpthread -lz -lm
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/Slugs'
(cd CAPS; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS'
/bin/cp Cart3D/X86_64_GCC/libc3dio.a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libc3dio.a
/bin/cp Cart3D/X86_64_GCC/libCart3D.a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libCart3D.a
/bin/cp Executables/LINUX64/avl /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/avl
/bin/cp Executables/LINUX64/pplot /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/pplot
/bin/cp Executables/LINUX64/pxplot /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/pxplot
/bin/cp Executables/LINUX64/xfoil /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/xfoil
/bin/cp Executables/LINUX64/mastros.exe /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/mastros.exe
/bin/cp Executables/LINUX64/ASTRO.D01 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/ASTRO.D01
/bin/cp Executables/LINUX64/ASTRO.IDX /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/ASTRO.IDX
/bin/cp Executables/LINUX64/mses /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/mses
/bin/cp Executables/LINUX64/mset /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/mset
/bin/cp udunits/include/*.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include
/bin/cp udunits/LINUX64/libudunits2.so /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib
ln -sf libudunits2.so /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libudunits2.so.0
/bin/cp Libraries/LINUX64/aflr2AIM.so /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/aflr2AIM.so
/bin/cp Libraries/LINUX64/aflr3AIM.so /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/aflr3AIM.so
/bin/cp Libraries/LINUX64/aflr4AIM.so /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/aflr4AIM.so
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS'
(cd CAPS/src; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/src'
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/caps.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/caps.h
cp -p ../include/caps.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/caps.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/capsErrors.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/capsErrors.h
cp -p ../include/capsErrors.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/capsErrors.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/capsTypes.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/capsTypes.h
cp -p ../include/capsTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/capsTypes.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aimUtil.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aimUtil.h
cp -p ../include/aimUtil.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aimUtil.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aimMesh.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aimMesh.h
cp -p ../include/aimMesh.h /home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../include \
	aimMesh.c -o ./aimMesh.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libaimUtil.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libaimUtil.a
ar -rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libaimUtil.a ./aimUtil.o ./aimMesh.o \
	./aimTransferUtil.o 
ar: creating /home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 printObject.c -o ./printObject.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libcaps.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libcaps.so
(cd .; gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/lib -ludunits2 -locsm -legads -ldl \
		-lrt -lm )
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libcapsstatic.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libcapsstatic.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.7/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/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include testingAIM.c \
	-o ./testingAIM.o
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingAIM.so
rm: cannot remove '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingAIM.so': No such file or directory
make[1]: [Makefile:23: /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingAIM.so] Error 1 (ignored)
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingAIM.so ./testingAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include testingWriter.c \
	-o ./testingWriter.o
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingWriter.so
rm: cannot remove '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingWriter.so': No such file or directory
make[1]: [Makefile:33: /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingWriter.so] Error 1 (ignored)
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingWriter.so ./testingWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include phaseUtil.c \
	-o ./phaseUtil.o
gcc -g  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/phaseUtil ./phaseUtil.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -ludunits2 -locsm -legads -ldl -lrt -lm
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/src'
(cd ../CAPSexamples; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples'
(make -C cCAPS -f aeroelastic_SU2.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include avlTest.c -o ./avlTest.o
gcc -g  -o ./avlTest ./avlTest.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include awaveTest.c -o ./awaveTest.o
gcc -g  -o ./awaveTest ./awaveTest.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include frictionTest.c -o ./frictionTest.o
gcc -g  -o ./frictionTest ./frictionTest.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include fun3dAFLR2Test.c -o ./fun3dAFLR2Test.o
gcc -g  -o ./fun3dAFLR2Test ./fun3dAFLR2Test.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include fun3dTetgenTest.c -o ./fun3dTetgenTest.o
gcc -g  -o ./fun3dTetgenTest ./fun3dTetgenTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include aeroelasticTest.c -o ./aeroelasticTest.o
gcc -g  -o ./aeroelasticTest ./aeroelasticTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f hsm.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include hsmTest.c -o ./hsmTest.o   
gcc -g  -o ./hsmTest ./hsmTest.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include hsmSimplePlateTest.c -o ./hsmSimplePlateTest.o  
gcc -g  -o ./hsmSimplePlateTest ./hsmSimplePlateTest.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include hsmCantileverPlateTest.c -o ./hsmCantileverPlateTest.o  
gcc -g  -o ./hsmCantileverPlateTest ./hsmCantileverPlateTest.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include hsmJoinedPlateTest.c -o ./hsmJoinedPlateTest.o  
gcc -g  -o ./hsmJoinedPlateTest ./hsmJoinedPlateTest.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include interferenceTest.c \
	-o ./interferenceTest.o   
gcc -g  -o ./interferenceTest ./interferenceTest.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include msesTest.c -o ./msesTest.o
gcc -g  -o ./msesTest ./msesTest.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f mystran.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include mystranTest.c -o ./mystranTest.o   
gcc -g  -o ./mystranTest ./mystranTest.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include pointwiseTest.c -o ./pointwiseTest.o
gcc -g  -o ./pointwiseTest ./pointwiseTest.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples'
(cd CAPS/aim; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim'
make -C utils
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. vlmSpanSpace.cpp -o ./vlmSpanSpace.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libutils.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libutils.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/lib/libutils.a
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils
cp -p -f attrUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/attrUtils.h
cp -p -f nastranCards.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/nastranCards.h
cp -p -f cfdTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/cfdTypes.h
cp -p -f arrayUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/arrayUtils.h
cp -p -f meshUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/meshUtils.h
cp -p -f feaTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/feaTypes.h
cp -p -f miscUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/miscUtils.h
cp -p -f meshTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/meshTypes.h
cp -p -f attrTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/attrTypes.h
cp -p -f vlmTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/vlmTypes.h
cp -p -f feaUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/feaUtils.h
cp -p -f cfdUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/cfdUtils.h
cp -p -f vlmUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/vlmUtils.h
cp -p -f cardTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/cardTypes.h
cp -p -f jsonUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/jsonUtils.h
cp -p -f nastranUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/nastranUtils.h
cp -p -f deprecateUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/deprecateUtils.h
cp -p -f miscTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/miscTypes.h
cp -p -f tecplotUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/tecplotUtils.h
cp -p -f vlmSpanSpace.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/vlmSpanSpace.h
cp -p -f cardUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/cardUtils.h
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/utils'
make -C friction 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -Wno-format -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils frictionAIM.c \
	-o ./frictionAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/frictionAIM.so ./frictionAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/bin/friction ./friction.o 
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/friction'
make -C tetgen 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/lib/tetgenAIM.so ./tetgenAIM.o \
	./tetgen_Interface.o ./tetgen.o \
	./predicates.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \
	-legads -ludunits2 -ldl -lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/tetgen'
make -C tacs 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils tacsAIM.c \
	-o ./tacsAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tacsAIM.so ./tacsAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/tacs'
make -C astros 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils astrosCards.c \
        -o ./astrosCards.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/astrosAIM.so ./astrosAIM.o  ./astrosUtils.o ./astrosCards.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/astros'
make -C pointwise 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils hashElement.c \
	-o ./hashElement.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pointwiseAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pointwiseAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pointwiseAIM.so ./pointwiseAIM.o ./hashElement.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
	-lrt -lm -lpthread
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/pointwise'
make -C xfoil 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils \
	xfoilAIM.c -o ./xfoilAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/xfoilAIM.so ./xfoilAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/xfoil'
make -C aflr2 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/aflr2'
make -C aflr4 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/aflr4'
make -C su2 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/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/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/su2'
make -C cgt 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include aflr4egads.c \
	-o ./aflr4egads.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/egads2cgt ./egads2cgt.o ./aflr4egads.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -legads -lcaps -locsm -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/cgt'
make -C mses 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils msesUtils.c -o msesUtils.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/msesAIM.so ./msesAIM.o ./msesUtils.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/mses'
make -C egadsTess 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils egadsTessAIM.c \
	-o ./egadsTessAIM.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/egadsTessAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/egadsTessAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/egadsTessAIM.so ./egadsTessAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
	-lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/egadsTess'
make -C sierraSD 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/sierraSD'
make -C masstran 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils masstranAIM.cpp \
	-o ./masstranAIM.o
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/masstranAIM.so ./masstranAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/masstran'
make -C plato 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/plato'
make -C refine 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 \
	-I../meshWriter/libmeshbWriter/libMeshb/sources \
	../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \
	-o ./libmeshb7.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/refineAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/refineAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/refineAIM.so ./refineAIM.o ./libmeshb7.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
	-lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/refine'
make -C awave 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils awaveAIM.c \
	-o ./awaveAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/awaveAIM.so ./awaveAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/awave'
make -C tsfoil 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils \
	tsfoilAIM.c -o ./tsfoilAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tsfoilAIM.so ./tsfoilAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/tsfoil'
make -C delaundo 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils delaundoAIM.c \
	-o ./delaundoAIM.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/delaundoAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/delaundoAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/delaundoAIM.so ./delaundoAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
	-lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/delaundo'
make -C abaqus 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/lib/abaqusAIM.so ./abaqusAIM.o ./abaqusUtils.o ./abaqusFILReader.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/abaqus'
make -C fun3d 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
	-I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
	-I/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/lib/fun3dAIM.so ./fun3dAIM.o ./fun3dUtils.o \
	./fun3dNamelist.o -L/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/fun3d'
make -C cbaero 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I. -I/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/lib/cbaeroAIM.so -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/cbaero'
make -C interference 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. cloudFns.c \
	-o ./cloudFns.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/interferenceAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/interferenceAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/interferenceAIM.so \
	./interferenceAIM.o ./cloudFns.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib \
	-laimUtil -locsm -legads -ludunits2 -ldl -lstdc++ -lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/interference'
make -C meshWriter 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter'
make -C libmeshbWriter 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7  -IlibMeshb/sources -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include libMeshb/sources/libmeshb7.c \
	-o ./libmeshb7.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libmeshbWriter.so ./libmeshbWriter.o ./libmeshb7.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/libmeshbWriter'
make -C fastWriter 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include fastWriter.c \
	-o ./fastWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/fastWriter.so ./fastWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/fastWriter'
make -C tecplotWriter 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include tecplotWriter.c \
	-o ./tecplotWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tecplotWriter.so ./tecplotWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/tecplotWriter'
make -C vtkWriter 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include vtkWriter.c \
	-o ./vtkWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vtkWriter.so ./vtkWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/vtkWriter'
make -C bstlWriter 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include bstlWriter.c \
	-o ./bstlWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bstlWriter.so ./bstlWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bstlWriter'
make -C bvtkWriter 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include bvtkWriter.c \
	-o ./bvtkWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bvtkWriter.so ./bvtkWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bvtkWriter'
make -C su2Writer 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include su2Writer.c \
	-o ./su2Writer.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/su2Writer.so ./su2Writer.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/su2Writer'
make -C stlWriter 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include stlWriter.c \
	-o ./stlWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stlWriter.so ./stlWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/stlWriter'
make -C ugridWriter 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include ugridWriter.c \
	-o ./ugridWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ugridWriter.so ./ugridWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/ugridWriter'
make -C exodusWriter 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/exodusWriter'
make[3]: Nothing to be done for 'default'.
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/exodusWriter'
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter'
make -C cart3d 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/cart3d'
make[2]: xml2-config: Command not found
XML developer libarary missing. Not compiling cart3dAIM.
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/cart3d'
make -C nastran 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils nastranAIM.c \
	-o ./nastranAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nastranAIM.so ./nastranAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/nastran'
make -C spinnaker 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/spinnaker'
make[2]: Nothing to be done for 'default'.
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/spinnaker'
make -C aflr3 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/aflr3'
make -C sierraSM 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/sierraSM'
make -C hsm 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 \
	-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=7.7 \
	-o src/genrcmi.o
make -C src hsmglr.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmbc.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmbb2.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmre1.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmdep.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmrfm.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmout.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmren.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmprj.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src atanc.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src cross.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src ludcmp.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmabd.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src bmdump.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmrun.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmeqn.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmsol.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmgeo.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src sbsolve.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libhsm.a
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libhsm.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libhsm.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/lib/libhsm.a
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/hsmAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/hsmAIM.so
gfortran -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \
	-legads -ludunits2 -lhsm -ldl  -lstdc++ 
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm'
make -C avl 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/lib/avlAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/avlAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \
	-lstdc++ -lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/avl'
make -C custom 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/custom'
make[2]: Nothing to be done for 'default'.
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/custom'
make -C skeleton 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils skeletonAIM.c \
	-o ./skeletonAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/skeletonAIM.so ./skeletonAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/skeleton'
make -C unitTest 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest'
make[2]: Nothing to be done for 'all'.
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest'
make -C mystran 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils mystranUtils.c \
	-o ./mystranUtils.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mystranAIM.so ./mystranAIM.o ./mystranUtils.o \
	-L/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/src/CAPS/aim/mystran'
make -C zaero 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils zaeroGraphical.c -o zaeroGraphical.o
gcc -g  -shared -Wl,-no-undefined   -o /home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/zaero'
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim'
(cd OpenCSM; make -f serveESP.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timCapsMode.c -o ./timCapsMode.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/capsMode.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/capsMode.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/capsMode.so ./timCapsMode.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timFlowchart.c -o ./timFlowchart.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/flowchart.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/flowchart.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/flowchart.so ./timFlowchart.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timViewer.c -o ./timViewer.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/viewer.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/viewer.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/viewer.so ./timViewer.o -L/home/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/EngSketchPad/lib/pyscript.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pyscript.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.7/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/7.7/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/7.7/LINUX64/EngSketchPad/src/OpenCSM'
 
 *** Build Completed! ***
+ export CSMDATA=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data
+ CSMDATA=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin
++ uname -a
+ [[ Linux reynolds-centOS8 4.18.0-552.el8.x86_64 #1 SMP Sun Apr 7 19:39:51 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/7.7/LINUX64/Verification.sh
+ bash -ex /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/Verification.sh
+ expectSuccess 01 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/expressions.vfy", so verification is being skipped
ERROR:: (func_arg_out_of_bounds) in Branch Brch_000152 at [[/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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	0m0.072s
user	0m0.054s
sys	0m0.017s
+ set +x

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

+ expectSuccess 02 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/demo2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/demo2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/demo2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.339s
user	0m0.474s
sys	0m0.023s
+ set +x

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

+ expectSuccess 03 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/tutorial1_whole
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/tutorial1_whole
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/verify_7.7.0/tutorial1_whole.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m2.607s
user	0m4.272s
sys	0m0.115s
+ set +x

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

+ expectSuccess 04 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/design2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/design2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/design2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.515s
user	0m0.745s
sys	0m0.022s
+ set +x

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

+ expectSuccess 05 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/design3
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/design3
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/design3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.417s
user	0m0.726s
sys	0m0.019s
+ set +x

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

+ expectSuccess 06 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/tutorial2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/tutorial2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/verify_7.7.0/tutorial2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.480s
user	0m0.810s
sys	0m0.020s
+ set +x

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

+ expectSuccess 07 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/tutorial3
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/tutorial3
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/verify_7.7.0/tutorial3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m3.120s
user	0m5.258s
sys	0m0.071s
+ set +x

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

+ expectSuccess 08 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/CAPS/myPlane
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/CAPS/myPlane
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/CAPS/verify_7.7.0/myPlane.vfy", so verification is being skipped
==> serveESP completed successfully with 12 warnings and no verification data

real	0m26.520s
user	0m45.087s
sys	0m0.205s
+ set +x

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

+ expectSuccess 09 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/bottle
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/bottle
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/verify_7.7.0/bottle.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.566s
user	0m0.670s
sys	0m0.016s
+ set +x

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

+ expectSuccess 10 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/wingMultiModel
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/wingMultiModel
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/wingMultiModel.vfy", so verification is being skipped
==> serveESP completed successfully with 4 warnings and no verification data

real	0m34.048s
user	1m0.109s
sys	0m1.060s
+ set +x

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

+ expectSuccess 11 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/bullet
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/bullet
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/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	0m0.281s
user	0m0.348s
sys	0m0.017s
+ set +x

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

+ expectSuccess 12 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/connect5
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/connect5
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/connect5.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.623s
user	0m0.950s
sys	0m0.020s
+ set +x

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

+ expectSuccess 13 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/group2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/group2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/group2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.184s
user	0m0.273s
sys	0m0.027s
+ set +x

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

+ expectSuccess 14 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/csm3
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/csm3
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/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	0m0.457s
user	0m0.658s
sys	0m0.026s
+ set +x

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

+ cd /home/jenkins/workspace/ESP_Beta/7.7/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 2.369s

OK
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/testOCSM
+ source /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/JenkinsESP/test_pyOCSM.sh
++ set -x
++ python -u test_pyOCSM.py -skipHelp

real	0m5.391s
user	0m9.807s
sys	0m0.120s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /home/jenkins/workspace/ESP_Beta/7.7/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 12.450s

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/7.7/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          =     0.067   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          =     0.122   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          =     0.001   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          =     0.072   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          =     0.110   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          =     0.001   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2244      2244
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       450       902
AFLR2 IG : Nodes, Faces      =       900      1802
AFLR2 IG : Nodes, Faces      =      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          =     0.076   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          =     0.120   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
 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          =     0.028   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          =     0.018   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          =     0.001   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2244      2244
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       450       902
AFLR2 IG : Nodes, Faces      =       900      1802
AFLR2 IG : Nodes, Faces      =      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          =     0.079   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          =     0.128   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
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          =     0.013   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      4705      9066
 
AFLR2    : CPU Time          =     0.002   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          =     0.015   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          =     0.008   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          =     0.014   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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 7):
	Number of nodes          = 6281
	Number of elements       = 34888
	Number of triangles      = 4448
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 30440
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 7):
	Number of nodes          = 13612
	Number of elements       = 76381
	Number of triangles      = 8144
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 68237
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 7):
	Number of nodes          = 41953
	Number of elements       = 238379
	Number of triangles      = 19880
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 218499
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 7):
	Number of nodes          = 4364
	Number of elements       = 24190
	Number of triangles      = 3016
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 21174
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh for body 6 (of 7):
	Number of nodes          = 11063
	Number of elements       = 61143
	Number of triangles      = 8630
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 52513
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh for body 7 (of 7):
	Number of nodes          = 10571
	Number of elements       = 59256
	Number of triangles      = 6368
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 52888
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 7 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 89033
	Number of elements       = 500486
	Number of triangles      = 51818
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 448668
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 16433
	Number of elements       = 93529
	Number of triangles      = 7926
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 85603
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 3645
	Number of elements       = 19765
	Number of triangles      = 3394
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 16371
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5471
	Number of elements       = 30418
	Number of triangles      = 3656
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 26762
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 4)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 4)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 4)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 7 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 7 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 8 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 9 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 10 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 11 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 12 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 13 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 14 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 15 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 16 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 17 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 18 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 19 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5077
	Number of elements       = 27808
	Number of triangles      = 4070
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 23738
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5223
	Number of elements       = 28360
	Number of triangles      = 4622
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 23738
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 2):
	Number of nodes          = 4887
	Number of elements       = 26853
	Number of triangles      = 4038
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 22815
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 33090
	Number of elements       = 191624
	Number of triangles      = 8496
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 183128
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 36430
	Number of elements       = 204952
	Number of triangles      = 21824
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 183128
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 5):
	Number of nodes          = 28936
	Number of elements       = 164394
	Number of triangles      = 15160
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 149234
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 5):
	Number of nodes          = 4115
	Number of elements       = 22780
	Number of triangles      = 2940
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 19840
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 16800
	Number of elements       = 95304
	Number of triangles      = 8802
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 86502
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 18724
	Number of elements       = 102680
	Number of triangles      = 16178
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 86502
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 2):
	Number of nodes          = 12168
	Number of elements       = 68392
	Number of triangles      = 7142
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 61250
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 2):
	Number of nodes          = 6556
	Number of elements       = 34288
	Number of triangles      = 9036
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 25252
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 6442
	Number of elements       = 36024
	Number of triangles      = 4052
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 31972
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 59849
	Number of elements       = 349298
	Number of triangles      = 12928
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 336370
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 59428
	Number of elements       = 346223
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 333795
	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 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 59849
	Number of elements       = 348798
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 336370
	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
 7F00C51A1740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F00C51A1740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7F00A70CC700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F00A70CC700 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
 7F00A70CC700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F00A70CC700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7F00C51A1740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F00C51A1740 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
 7F00A68CB700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F00A68CB700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7F00C51A1740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F00C51A1740 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
 7F00A60CA700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F00A60CA700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7F00A70CC700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F00A70CC700 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:  0.148887
Creating surface mesh ...
Surface mesh seconds:  0.037253
Recovering boundaries...
Boundary recovery seconds:  0.164358
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.071085
Recovering Delaunayness...
Delaunay recovery seconds:  0.074751
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:  2.93421
Smoothing vertices...
Mesh smoothing seconds:  2.6793
Improving mesh...
Mesh improvement seconds:  0.057388

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

Output seconds:  0.015658
Total running seconds:  6.18349

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:  0.154748
Creating surface mesh ...
Surface mesh seconds:  0.037502
Recovering boundaries...
Boundary recovery seconds:  0.169861
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.072728
Recovering Delaunayness...
Delaunay recovery seconds:  0.075514
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:  2.91766
Smoothing vertices...
Mesh smoothing seconds:  2.57805
Improving mesh...
Mesh improvement seconds:  0.057331

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

Output seconds:  0.016266
Total running seconds:  6.08028

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/7.7/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/7.7/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/7.7/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
*** ERROR 200212 : duplicate boundary edges found ***
ERROR
test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ... *** ERROR 200212 : duplicate boundary edges found ***
FAIL
test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ... *** ERROR 200212 : duplicate boundary edges found ***
FAIL
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
*** ERROR 200212 : duplicate boundary edges found ***
ERROR
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
*** ERROR 200212 : duplicate boundary edges found ***
ERROR
test_reenter (test_su2.TestSU2.test_reenter) ... *** ERROR 200212 : duplicate boundary edges found ***
ERROR
test_units (test_su2.TestSU2.test_units) ... *** ERROR 200212 : duplicate boundary edges found ***
ERROR
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)
 7F00A70CC700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F00A70CC700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7F00A60CA700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F00A60CA700 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
 caps_filter Warning: No bodies with capsAIM = tetgenAIM!
   Body 1 capsAIM = aflr4AIM;aflr3AIM;platoAIM
   Body 2 capsAIM = aflr4AIM;aflr3AIM;platoAIM
 caps_filter Warning: No bodies with capsAIM = egadsTessAIM!
   Body 1 capsAIM = aflr4AIM;aflr3AIM;platoAIM
   Body 2 capsAIM = aflr4AIM;aflr3AIM;platoAIM
ERROR
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

======================================================================
ERROR: test_inputs (test_su2.TestSU2.test_inputs)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 102, in test_inputs
    self.myAnalysis.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error):
================================================================================
aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212
aflr4_Interface.c:588 in aflr4_Surface_Mesh():
  Error: AFLR4 mesh generation failed...
  An EGADS file with all AFLR4 parameters
  has been written to 'aflr4_debug.egads'
aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212
  Problem during AFLR4 surface meshing
transferValues for Surface_Mesh from Surface_Mesh = 200212
transferValues for Mesh from Volume_Mesh = 200212
================================================================================


======================================================================
ERROR: test_journal (test_su2.TestSU2.test_journal)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 357, in test_journal
    line_total = self.run_journal(myProblem, -1)
                 ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 310, in run_journal
    su2.preAnalysis(); line += 1
    ^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error):
================================================================================
aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212
aflr4_Interface.c:588 in aflr4_Surface_Mesh():
  Error: AFLR4 mesh generation failed...
  An EGADS file with all AFLR4 parameters
  has been written to 'aflr4_debug.egads'
aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212
  Problem during AFLR4 surface meshing
transferValues for Surface_Mesh from Surface_Mesh = 200212
transferValues for Mesh from Volume_Mesh = 200212
================================================================================


======================================================================
ERROR: test_phase (test_su2.TestSU2.test_phase)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 226, in test_phase
    su2.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error):
================================================================================
aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212
aflr4_Interface.c:588 in aflr4_Surface_Mesh():
  Error: AFLR4 mesh generation failed...
  An EGADS file with all AFLR4 parameters
  has been written to 'aflr4_debug.egads'
aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212
  Problem during AFLR4 surface meshing
transferValues for Surface_Mesh from Surface_Mesh = 200212
transferValues for Mesh from Volume_Mesh = 200212
================================================================================


======================================================================
ERROR: test_reenter (test_su2.TestSU2.test_reenter)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 152, in test_reenter
    self.myAnalysis.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error):
================================================================================
aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212
aflr4_Interface.c:588 in aflr4_Surface_Mesh():
  Error: AFLR4 mesh generation failed...
  An EGADS file with all AFLR4 parameters
  has been written to 'aflr4_debug.egads'
aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212
  Problem during AFLR4 surface meshing
transferValues for Surface_Mesh from Surface_Mesh = 200212
transferValues for Mesh from Volume_Mesh = 200212
================================================================================


======================================================================
ERROR: test_units (test_su2.TestSU2.test_units)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 194, in test_units
    myAnalysis.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error):
================================================================================
aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212
aflr4_Interface.c:588 in aflr4_Surface_Mesh():
  Error: AFLR4 mesh generation failed...
  An EGADS file with all AFLR4 parameters
  has been written to 'aflr4_debug.egads'
aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212
  Problem during AFLR4 surface meshing
transferValues for Surface_Mesh from Surface_Mesh = 200212
transferValues for Mesh from Volume_Mesh = 200212
================================================================================


======================================================================
ERROR: test_faceMatch_MultiDomain (test_tetgen.TestTETGEN.test_faceMatch_MultiDomain)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_tetgen.py", line 167, in test_faceMatch_MultiDomain
    tetgen.runAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2144, in runAnalysis
    self._analysisObj.execute()
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2901, in execute
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_SOURCEERR:
================================================================================
egadsTessAIM.c:420 in aimUpdateState():
  Error: No Bodies!
transferValues for Surface_Mesh from Surface_Mesh = -330
================================================================================


======================================================================
FAIL: test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 142, in test_invalidBoundary
    self.assertEqual(e.exception.errorName, "CAPS_NOTFOUND")
AssertionError: 'UNKNOWN_ERROR' != 'CAPS_NOTFOUND'
- UNKNOWN_ERROR
+ CAPS_NOTFOUND


======================================================================
FAIL: test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 124, in test_invalidBoundaryName
    self.assertEqual(e.exception.errorName, "CAPS_NOTFOUND")
AssertionError: 'UNKNOWN_ERROR' != 'CAPS_NOTFOUND'
- UNKNOWN_ERROR
+ CAPS_NOTFOUND


----------------------------------------------------------------------
Ran 143 tests in 442.879s

FAILED (failures=2, errors=6, skipped=26)
 CAPS Error: Cannot open /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/su2_problem/Scratch/capsRestart/Problem!
 CAPS Warning: caps_writeProblem = -333 (caps_close)!
make: *** [Makefile:4: test] Error 1
Build step 'Conditional step (single)' marked build as failure
[GNU C Compiler (gcc)Clang] Skipping execution of recorder since overall result is 'FAILURE'
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Skipped based on build state FAILURE
Finished: FAILURE