Console Output

Started by upstream project "ESP_Beta" build number 732
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/7.8/LINUX64
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
Checking out a fresh workspace because there's no workspace at /home/jenkins/workspace/ESP_Beta/7.8/LINUX64
Cleaning local Directory .
Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-06-25T22:58:15.774 -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 2508

Checking out a fresh workspace because /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP doesn't exist
Cleaning local Directory JenkinsESP
Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-06-25T22:58:15.774 -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 875

No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
[GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[Execution node] check if [reynolds-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/jenkins1682557036173324266.sh
+ bash -ex /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/ESP_Beta.sh
+ source /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.8
++ OCCTREF=7.8
++ AFLR_VERSION=11.5.14
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.38.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ export MPLBACKEND=agg
++ MPLBACKEND=agg
++ 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 46436 172.16.90.130 22' ']'
+++++ '[' -z 14 ']'
+++++ '[' -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/2941663/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/7.8/LINUX64/ESP/LINUX64
++ ESP_BLOC=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64
++ export ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64
++ ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64
++ export JULIA_DEPOT_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/julia
++ JULIA_DEPOT_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.8 != '' ]]
++ [[ '' != '' ]]
++ [[ reynolds-centOS8 == *\r\e\y\n\o\l\d\s* ]]
++ [[ '' != '' ]]
++ [[ -d /home/jenkins/util/ESP/Python/ESP_Python-3.11.9 ]]
++ export PYTHONHOME=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9
++ PYTHONHOME=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9
++ export PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/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-7.8.0
++ export CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export CASARCH=.
++ CASARCH=.
++ export LD_LIBRARY_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ LD_LIBRARY_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ export ESP_EXTERN_LIBS=/home/jenkins/util/ESP/ExternLibs
++ ESP_EXTERN_LIBS=/home/jenkins/util/ESP/ExternLibs
++ export AFLR=/home/jenkins/util/AFLR/aflr_lib_11.5.14
++ AFLR=/home/jenkins/util/AFLR/aflr_lib_11.5.14
++ export AFLR_ARCH=Linux-x86-64
++ AFLR_ARCH=Linux-x86-64
++ export PATH=/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/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/7.8/LINUX64/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/aim/pointwise/glyph
++ export PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/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/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/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/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/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/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/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/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/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/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ [[ reynolds-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/7.8/LINUX64/OpenCSM/trunk/data
++ CSMDATA=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/data
+ virtualenv /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv
created virtual environment CPython3.11.9.final.0-64 in 482ms
  creator CPython3Posix(dest=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv, clear=False, no_vcs_ignore=False, global=False)
  seeder FromAppData(download=False, pip=bundle, setuptools=bundle, wheel=bundle, via=copy, app_data_dir=/home/jenkins/.local/share/virtualenv)
    added seed packages: pip==24.0, setuptools==70.0.0, wheel==0.43.0
  activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator
+ . /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/activate
++ '[' /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/activate = /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/ESP_Beta.sh ']'
++ deactivate nondestructive
++ unset -f pydoc
++ '[' -z '' ']'
++ '[' -z '' ']'
++ hash -r
++ '[' -z '' ']'
++ unset VIRTUAL_ENV
++ unset VIRTUAL_ENV_PROMPT
++ '[' '!' nondestructive = nondestructive ']'
++ VIRTUAL_ENV=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv
++ '[' linux-gnu = cygwin ']'
++ '[' linux-gnu = msys ']'
++ export VIRTUAL_ENV
++ _OLD_VIRTUAL_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/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/7.8/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/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/7.8/LINUX64/ESP_venv
++ VIRTUAL_ENV_PROMPT=ESP_venv
++ export VIRTUAL_ENV_PROMPT
++ '[' -z _ ']'
++ _OLD_VIRTUAL_PYTHONHOME=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9
++ unset PYTHONHOME
++ '[' -z '' ']'
++ _OLD_VIRTUAL_PS1=
++ PS1='(ESP_venv) '
++ export PS1
++ alias pydoc
++ true
++ hash -r
+ pip_install pip
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade pip
Requirement already satisfied: pip in ./ESP_venv/lib/python3.11/site-packages (24.0)
Collecting pip
  Using cached pip-24.1-py3-none-any.whl.metadata (3.6 kB)
Using cached pip-24.1-py3-none-any.whl (1.8 MB)
Installing collected packages: pip
  Attempting uninstall: pip
    Found existing installation: pip 24.0
    Uninstalling pip-24.0:
      Successfully uninstalled pip-24.0
Successfully installed pip-24.1
+ pip_install f90nml
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade f90nml
Collecting f90nml
  Using cached f90nml-1.4.4-py2.py3-none-any.whl.metadata (6.0 kB)
Using cached f90nml-1.4.4-py2.py3-none-any.whl (32 kB)
Installing collected packages: f90nml
Successfully installed f90nml-1.4.4
+ pip_install numpy
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade numpy
Collecting numpy
  Using cached numpy-2.0.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (60 kB)
Using cached numpy-2.0.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (19.3 MB)
Installing collected packages: numpy
Successfully installed numpy-2.0.0
+ pip_install openmdao
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade openmdao
Collecting openmdao
  Using cached openmdao-3.33.0-py3-none-any.whl
Collecting networkx>=2.0 (from openmdao)
  Using cached networkx-3.3-py3-none-any.whl.metadata (5.1 kB)
Collecting numpy<2 (from openmdao)
  Using cached numpy-1.26.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (61 kB)
Collecting packaging (from openmdao)
  Using cached packaging-24.1-py3-none-any.whl.metadata (3.2 kB)
Collecting requests (from openmdao)
  Using cached requests-2.32.3-py3-none-any.whl.metadata (4.6 kB)
Collecting scipy (from openmdao)
  Using cached scipy-1.14.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (60 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 urllib3-2.2.2-py3-none-any.whl.metadata (6.4 kB)
Collecting certifi>=2017.4.17 (from requests->openmdao)
  Using cached certifi-2024.6.2-py3-none-any.whl.metadata (2.2 kB)
Using cached networkx-3.3-py3-none-any.whl (1.7 MB)
Using cached numpy-1.26.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (18.3 MB)
Using cached packaging-24.1-py3-none-any.whl (53 kB)
Using cached requests-2.32.3-py3-none-any.whl (64 kB)
Using cached scipy-1.14.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (41.1 MB)
Using cached certifi-2024.6.2-py3-none-any.whl (164 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 urllib3-2.2.2-py3-none-any.whl (121 kB)
Installing collected packages: urllib3, packaging, numpy, networkx, idna, charset-normalizer, certifi, scipy, requests, openmdao
  Attempting uninstall: numpy
    Found existing installation: numpy 2.0.0
    Uninstalling numpy-2.0.0:
      Successfully uninstalled numpy-2.0.0
Successfully installed certifi-2024.6.2 charset-normalizer-3.3.2 idna-3.7 networkx-3.3 numpy-1.26.4 openmdao-3.33.0 packaging-24.1 requests-2.32.3 scipy-1.14.0 urllib3-2.2.2
+ [[ reynolds-centOS8 == *\v\i\g\g\e\n* ]]
+ pip_install cvxopt
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade cvxopt
Collecting cvxopt
  Using cached cvxopt-1.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (1.3 kB)
Using cached cvxopt-1.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (13.6 MB)
Installing collected packages: cvxopt
Successfully installed cvxopt-1.3.2
+ pip_install dill
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade dill
Collecting dill
  Using cached dill-0.3.8-py3-none-any.whl.metadata (10 kB)
Using cached dill-0.3.8-py3-none-any.whl (116 kB)
Installing collected packages: dill
Successfully installed dill-0.3.8
+ pip_install packaging
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade packaging
Requirement already satisfied: packaging in ./ESP_venv/lib/python3.11/site-packages (24.1)
+ pip_install matplotlib
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade matplotlib
Collecting matplotlib
  Using cached matplotlib-3.9.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (11 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-4.53.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (162 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>=1.23 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) (24.1)
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-3.9.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (8.3 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-4.53.0-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)
Using cached pyparsing-3.1.2-py3-none-any.whl (103 kB)
Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl (229 kB)
Using cached six-1.16.0-py2.py3-none-any.whl (11 kB)
Installing collected packages: six, pyparsing, pillow, kiwisolver, fonttools, cycler, contourpy, python-dateutil, matplotlib
Successfully installed contourpy-1.2.1 cycler-0.12.1 fonttools-4.53.0 kiwisolver-1.4.5 matplotlib-3.9.0 pillow-10.3.0 pyparsing-3.1.2 python-dateutil-2.9.0.post0 six-1.16.0
+ pip_install scipy
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade scipy
Requirement already satisfied: scipy in ./ESP_venv/lib/python3.11/site-packages (1.14.0)
Requirement already satisfied: numpy<2.3,>=1.23.5 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
--2024-06-25 22:59:06--  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: 272186226 (260M) [application/x-gzip]
Saving to: ‘ESPbeta.tgz’

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 11100K .......... .......... .......... .......... ..........  4% 12.5M 13s
 11150K .......... .......... .......... .......... ..........  4% 16.3M 13s
 11200K .......... .......... .......... .......... ..........  4% 14.3M 13s
 11250K .......... .......... .......... .......... ..........  4% 14.4M 13s
 11300K .......... .......... .......... .......... ..........  4% 14.4M 13s
 11350K .......... .......... .......... .......... ..........  4% 10.3M 13s
 11400K .......... .......... .......... .......... ..........  4% 20.3M 13s
 11450K .......... .......... .......... .......... ..........  4% 10.8M 13s
 11500K .......... .......... .......... .......... ..........  4% 17.7M 13s
 11550K .......... .......... .......... .......... ..........  4% 14.7M 13s
 11600K .......... .......... .......... .......... ..........  4% 13.4M 13s
 11650K .......... .......... .......... .......... ..........  4% 29.6M 13s
 11700K .......... .......... .......... .......... ..........  4% 15.0M 13s
 11750K .......... .......... .......... .......... ..........  4% 15.0M 13s
 11800K .......... .......... .......... .......... ..........  4% 16.4M 13s
 11850K .......... .......... .......... .......... ..........  4% 23.7M 13s
 11900K .......... .......... .......... .......... ..........  4% 16.6M 13s
 11950K .......... .......... .......... .......... ..........  4% 15.0M 13s
 12000K .......... .......... .......... .......... ..........  4% 24.2M 13s
 12050K .......... .......... .......... .......... ..........  4% 14.0M 13s
 12100K .......... .......... .......... .......... ..........  4% 18.2M 13s
 12150K .......... .......... .......... .......... ..........  4% 14.7M 13s
 12200K .......... .......... .......... .......... ..........  4% 15.1M 13s
 12250K .......... .......... .......... .......... ..........  4% 29.2M 13s
 12300K .......... .......... .......... .......... ..........  4% 14.4M 13s
 12350K .......... .......... .......... .......... ..........  4% 13.2M 13s
 12400K .......... .......... .......... .......... ..........  4% 25.3M 13s
 12450K .......... .......... .......... .......... ..........  4% 14.5M 13s
 12500K .......... .......... .......... .......... ..........  4% 21.3M 13s
 12550K .......... .......... .......... .......... ..........  4% 14.6M 13s
 12600K .......... .......... .......... .......... ..........  4% 23.6M 13s
 12650K .......... .......... .......... .......... ..........  4% 14.2M 13s
 12700K .......... .......... .......... .......... ..........  4% 17.5M 13s
 12750K .......... .......... .......... .......... ..........  4% 16.1M 13s
 12800K .......... .......... .......... .......... ..........  4% 19.7M 13s
 12850K .......... .......... .......... .......... ..........  4% 17.8M 13s
 12900K .......... .......... .......... .......... ..........  4% 15.3M 13s
 12950K .......... .......... .......... .......... ..........  4% 17.0M 13s
 13000K .......... .......... .......... .......... ..........  4% 15.8M 13s
 13050K .......... .......... .......... .......... ..........  4% 30.6M 13s
 13100K .......... .......... .......... .......... ..........  4% 14.3M 13s
 13150K .......... .......... .......... .......... ..........  4% 15.1M 13s
 13200K .......... .......... .......... .......... ..........  4% 24.2M 13s
 13250K .......... .......... .......... .......... ..........  5% 16.7M 13s
 13300K .......... .......... .......... .......... ..........  5% 24.7M 13s
 13350K .......... .......... .......... .......... ..........  5% 18.9M 13s
 13400K .......... .......... .......... .......... ..........  5% 14.8M 13s
 13450K .......... .......... .......... .......... ..........  5% 22.5M 13s
 13500K .......... .......... .......... .......... ..........  5% 25.4M 13s
 13550K .......... .......... .......... .......... ..........  5% 16.7M 13s
 13600K .......... .......... .......... .......... ..........  5% 15.3M 13s
 13650K .......... .......... .......... .......... ..........  5% 23.0M 13s
 13700K .......... .......... .......... .......... ..........  5% 20.4M 13s
 13750K .......... .......... .......... .......... ..........  5% 21.7M 13s
 13800K .......... .......... .......... .......... ..........  5% 26.5M 13s
 13850K .......... .......... .......... .......... ..........  5% 15.0M 13s
 13900K .......... .......... .......... .......... ..........  5% 41.9M 13s
 13950K .......... .......... .......... .......... ..........  5% 14.6M 13s
 14000K .......... .......... .......... .......... ..........  5% 26.2M 13s
 14050K .......... .......... .......... .......... ..........  5% 26.7M 13s
 14100K .......... .......... .......... .......... ..........  5% 10.1M 13s
 14150K .......... .......... .......... .......... ..........  5%  104M 13s
 14200K .......... .......... .......... .......... ..........  5% 15.8M 13s
 14250K .......... .......... .......... .......... ..........  5% 35.6M 13s
 14300K .......... .......... .......... .......... ..........  5% 15.0M 13s
 14350K .......... .......... .......... .......... ..........  5% 15.6M 13s
 14400K .......... .......... .......... .......... ..........  5% 15.7M 13s
 14450K .......... .......... .......... .......... ..........  5% 15.8M 13s
 14500K .......... .......... .......... .......... ..........  5% 18.3M 13s
 14550K .......... .......... .......... .......... ..........  5% 16.9M 13s
 14600K .......... .......... .......... .......... ..........  5% 15.7M 13s
 14650K .......... .......... .......... .......... ..........  5% 8.85M 13s
 14700K .......... .......... .......... .......... ..........  5% 27.9M 13s
 14750K .......... .......... .......... .......... ..........  5% 20.5M 13s
 14800K .......... .......... .......... .......... ..........  5% 17.3M 13s
 14850K .......... .......... .......... .......... ..........  5% 13.7M 13s
 14900K .......... .......... .......... .......... ..........  5% 21.1M 13s
 14950K .......... .......... .......... .......... ..........  5% 10.6M 13s
 15000K .......... .......... .......... .......... ..........  5% 19.0M 13s
 15050K .......... .......... .......... .......... ..........  5% 18.8M 13s
 15100K .......... .......... .......... .......... ..........  5% 15.6M 13s
 15150K .......... .......... .......... .......... ..........  5% 22.6M 13s
 15200K .......... .......... .......... .......... ..........  5% 17.6M 13s
 15250K .......... .......... .......... .......... ..........  5% 18.8M 13s
 15300K .......... .......... .......... .......... ..........  5% 14.3M 13s
 15350K .......... .......... .......... .......... ..........  5% 12.0M 13s
 15400K .......... .......... .......... .......... ..........  5% 12.4M 13s
 15450K .......... .......... .......... .......... ..........  5% 23.2M 13s
 15500K .......... .......... .......... .......... ..........  5% 16.0M 13s
 15550K .......... .......... .......... .......... ..........  5% 20.0M 13s
 15600K .......... .......... .......... .......... ..........  5% 10.7M 13s
 15650K .......... .......... .......... .......... ..........  5% 20.1M 13s
 15700K .......... .......... .......... .......... ..........  5% 10.5M 13s
 15750K .......... .......... .......... .......... ..........  5% 19.2M 13s
 15800K .......... .......... .......... .......... ..........  5% 19.4M 13s
 15850K .......... .......... .......... .......... ..........  5% 16.5M 13s
 15900K .......... .......... .......... .......... ..........  6% 15.7M 13s
 15950K .......... .......... .......... .......... ..........  6% 17.5M 13s
 16000K .......... .......... .......... .......... ..........  6% 17.3M 13s
 16050K .......... .......... .......... .......... ..........  6% 19.6M 13s
 16100K .......... .......... .......... .......... ..........  6% 22.3M 13s
 16150K .......... .......... .......... .......... ..........  6% 24.6M 13s
 16200K .......... .......... .......... .......... ..........  6% 21.8M 13s
 16250K .......... .......... .......... .......... ..........  6% 26.5M 13s
 16300K .......... .......... .......... .......... ..........  6% 53.9M 13s
 16350K .......... .......... .......... .......... ..........  6% 19.6M 13s
 16400K .......... .......... .......... .......... ..........  6% 18.1M 13s
 16450K .......... .......... .......... .......... ..........  6% 16.9M 13s
 16500K .......... .......... .......... .......... ..........  6% 26.1M 13s
 16550K .......... .......... .......... .......... ..........  6% 28.5M 13s
 16600K .......... .......... .......... .......... ..........  6% 15.7M 13s
 16650K .......... .......... .......... .......... ..........  6% 25.3M 13s
 16700K .......... .......... .......... .......... ..........  6% 19.8M 13s
 16750K .......... .......... .......... .......... ..........  6% 33.0M 13s
 16800K .......... .......... .......... .......... ..........  6% 35.6M 13s
 16850K .......... .......... .......... .......... ..........  6% 16.1M 13s
 16900K .......... .......... .......... .......... ..........  6% 20.6M 13s
 16950K .......... .......... .......... .......... ..........  6% 22.5M 13s
 17000K .......... .......... .......... .......... ..........  6% 20.3M 13s
 17050K .......... .......... .......... .......... ..........  6% 21.6M 13s
 17100K .......... .......... .......... .......... ..........  6% 22.4M 13s
 17150K .......... .......... .......... .......... ..........  6% 23.3M 13s
 17200K .......... .......... .......... .......... ..........  6% 19.8M 13s
 17250K .......... .......... .......... .......... ..........  6% 21.6M 13s
 17300K .......... .......... .......... .......... ..........  6% 26.4M 13s
 17350K .......... .......... .......... .......... ..........  6% 24.2M 13s
 17400K .......... .......... .......... .......... ..........  6% 33.8M 13s
 17450K .......... .......... .......... .......... ..........  6% 11.7M 13s
 17500K .......... .......... .......... .......... ..........  6%  137M 13s
 17550K .......... .......... .......... .......... ..........  6% 15.9M 13s
 17600K .......... .......... .......... .......... ..........  6% 16.5M 13s
 17650K .......... .......... .......... .......... ..........  6% 18.4M 13s
 17700K .......... .......... .......... .......... ..........  6% 13.7M 13s
 17750K .......... .......... .......... .......... ..........  6% 14.9M 13s
 17800K .......... .......... .......... .......... ..........  6% 22.4M 13s
 17850K .......... .......... .......... .......... ..........  6% 11.2M 13s
 17900K .......... .......... .......... .......... ..........  6% 14.6M 13s
 17950K .......... .......... .......... .......... ..........  6% 8.93M 13s
 18000K .......... .......... .......... .......... ..........  6% 12.2M 13s
 18050K .......... .......... .......... .......... ..........  6% 9.92M 13s
 18100K .......... .......... .......... .......... ..........  6% 8.38M 13s
 18150K .......... .......... .......... .......... ..........  6% 7.78M 13s
 18200K .......... .......... .......... .......... ..........  6% 7.41M 13s
 18250K .......... .......... .......... .......... ..........  6% 6.81M 13s
 18300K .......... .......... .......... .......... ..........  6% 9.62M 13s
 18350K .......... .......... .......... .......... ..........  6% 9.85M 13s
 18400K .......... .......... .......... .......... ..........  6% 10.6M 13s
 18450K .......... .......... .......... .......... ..........  6% 11.7M 13s
 18500K .......... .......... .......... .......... ..........  6% 16.7M 13s
 18550K .......... .......... .......... .......... ..........  6% 10.9M 13s
 18600K .......... .......... .......... .......... ..........  7% 11.8M 14s
 18650K .......... .......... .......... .......... ..........  7% 14.7M 14s
 18700K .......... .......... .......... .......... ..........  7% 11.1M 14s
 18750K .......... .......... .......... .......... ..........  7% 15.4M 14s
 18800K .......... .......... .......... .......... ..........  7% 14.6M 14s
 18850K .......... .......... .......... .......... ..........  7% 18.7M 14s
 18900K .......... .......... .......... .......... ..........  7% 15.8M 14s
 18950K .......... .......... .......... .......... ..........  7% 23.0M 14s
 19000K .......... .......... .......... .......... ..........  7% 17.6M 14s
 19050K .......... .......... .......... .......... ..........  7% 51.9M 14s
 19100K .......... .......... .......... .......... ..........  7% 13.4M 14s
 19150K .......... .......... .......... .......... ..........  7% 66.2M 13s
 19200K .......... .......... .......... .......... ..........  7% 12.4M 13s
 19250K .......... .......... .......... .......... ..........  7% 37.2M 13s
 19300K .......... .......... .......... .......... ..........  7% 19.8M 13s
 19350K .......... .......... .......... .......... ..........  7% 13.5M 13s
 19400K .......... .......... .......... .......... ..........  7% 22.2M 13s
 19450K .......... .......... .......... .......... ..........  7% 20.4M 13s
 19500K .......... .......... .......... .......... ..........  7% 19.8M 13s
 19550K .......... .......... .......... .......... ..........  7% 26.2M 13s
 19600K .......... .......... .......... .......... ..........  7% 15.6M 13s
 19650K .......... .......... .......... .......... ..........  7% 19.8M 13s
 19700K .......... .......... .......... .......... ..........  7% 18.3M 13s
 19750K .......... .......... .......... .......... ..........  7% 17.2M 13s
 19800K .......... .......... .......... .......... ..........  7% 13.5M 13s
 19850K .......... .......... .......... .......... ..........  7% 10.4M 13s
 19900K .......... .......... .......... .......... ..........  7% 17.1M 13s
 19950K .......... .......... .......... .......... ..........  7% 14.4M 13s
 20000K .......... .......... .......... .......... ..........  7% 10.6M 13s
 20050K .......... .......... .......... .......... ..........  7% 14.6M 13s
 20100K .......... .......... .......... .......... ..........  7% 12.4M 14s
 20150K .......... .......... .......... .......... ..........  7% 13.2M 14s
 20200K .......... .......... .......... .......... ..........  7% 15.9M 14s
 20250K .......... .......... .......... .......... ..........  7% 12.9M 14s
 20300K .......... .......... .......... .......... ..........  7% 17.0M 14s
 20350K .......... .......... .......... .......... ..........  7% 18.1M 14s
 20400K .......... .......... .......... .......... ..........  7% 13.5M 14s
 20450K .......... .......... .......... .......... ..........  7% 22.2M 14s
 20500K .......... .......... .......... .......... ..........  7% 15.6M 14s
 20550K .......... .......... .......... .......... ..........  7% 16.1M 14s
 20600K .......... .......... .......... .......... ..........  7% 12.2M 14s
 20650K .......... .......... .......... .......... ..........  7% 16.5M 14s
 20700K .......... .......... .......... .......... ..........  7% 20.3M 14s
 20750K .......... .......... .......... .......... ..........  7% 12.1M 14s
 20800K .......... .......... .......... .......... ..........  7% 17.1M 14s
 20850K .......... .......... .......... .......... ..........  7% 22.7M 14s
 20900K .......... .......... .......... .......... ..........  7% 13.4M 14s
 20950K .......... .......... .......... .......... ..........  7% 20.3M 14s
 21000K .......... .......... .......... .......... ..........  7% 24.1M 14s
 21050K .......... .......... .......... .......... ..........  7% 23.3M 14s
 21100K .......... .......... .......... .......... ..........  7% 21.0M 13s
 21150K .......... .......... .......... .......... ..........  7% 19.8M 13s
 21200K .......... .......... .......... .......... ..........  7% 19.5M 13s
 21250K .......... .......... .......... .......... ..........  8% 18.7M 13s
 21300K .......... .......... .......... .......... ..........  8% 23.7M 13s
 21350K .......... .......... .......... .......... ..........  8% 18.9M 13s
 21400K .......... .......... .......... .......... ..........  8% 28.1M 13s
 21450K .......... .......... .......... .......... ..........  8% 20.6M 13s
 21500K .......... .......... .......... .......... ..........  8% 22.8M 13s
 21550K .......... .......... .......... .......... ..........  8% 18.3M 13s
 21600K .......... .......... .......... .......... ..........  8% 19.4M 13s
 21650K .......... .......... .......... .......... ..........  8% 21.3M 13s
 21700K .......... .......... .......... .......... ..........  8% 17.2M 13s
 21750K .......... .......... .......... .......... ..........  8% 18.6M 13s
 21800K .......... .......... .......... .......... ..........  8% 22.9M 13s
 21850K .......... .......... .......... .......... ..........  8% 20.7M 13s
 21900K .......... .......... .......... .......... ..........  8% 39.3M 13s
 21950K .......... .......... .......... .......... ..........  8% 9.29M 13s
 22000K .......... .......... .......... .......... ..........  8%  218M 13s
 22050K .......... .......... .......... .......... ..........  8% 21.6M 13s
 22100K .......... .......... .......... .......... ..........  8% 24.8M 13s
 22150K .......... .......... .......... .......... ..........  8% 16.1M 13s
 22200K .......... .......... .......... .......... ..........  8% 38.4M 13s
 22250K .......... .......... .......... .......... ..........  8% 18.3M 13s
 22300K .......... .......... .......... .......... ..........  8% 23.3M 13s
 22350K .......... .......... .......... .......... ..........  8% 24.0M 13s
 22400K .......... .......... .......... .......... ..........  8% 29.8M 13s
 22450K .......... .......... .......... .......... ..........  8% 15.5M 13s
 22500K .......... .......... .......... .......... ..........  8% 28.7M 13s
 22550K .......... .......... .......... .......... ..........  8% 30.5M 13s
 22600K .......... .......... .......... .......... ..........  8% 24.3M 13s
 22650K .......... .......... .......... .......... ..........  8% 23.5M 13s
 22700K .......... .......... .......... .......... ..........  8% 13.6M 13s
 22750K .......... .......... .......... .......... ..........  8% 22.2M 13s
 22800K .......... .......... .......... .......... ..........  8% 20.5M 13s
 22850K .......... .......... .......... .......... ..........  8% 14.5M 13s
 22900K .......... .......... .......... .......... ..........  8% 21.4M 13s
 22950K .......... .......... .......... .......... ..........  8% 18.0M 13s
 23000K .......... .......... .......... .......... ..........  8% 17.2M 13s
 23050K .......... .......... .......... .......... ..........  8% 17.6M 13s
 23100K .......... .......... .......... .......... ..........  8% 9.44M 13s
 23150K .......... .......... .......... .......... ..........  8% 18.0M 13s
 23200K .......... .......... .......... .......... ..........  8% 11.3M 13s
 23250K .......... .......... .......... .......... ..........  8% 15.8M 13s
 23300K .......... .......... .......... .......... ..........  8% 14.1M 13s
 23350K .......... .......... .......... .......... ..........  8% 15.6M 13s
 23400K .......... .......... .......... .......... ..........  8% 16.7M 13s
 23450K .......... .......... .......... .......... ..........  8% 15.3M 13s
 23500K .......... .......... .......... .......... ..........  8% 17.8M 13s
 23550K .......... .......... .......... .......... ..........  8% 17.1M 13s
 23600K .......... .......... .......... .......... ..........  8% 13.8M 13s
 23650K .......... .......... .......... .......... ..........  8% 14.8M 13s
 23700K .......... .......... .......... .......... ..........  8% 17.2M 13s
 23750K .......... .......... .......... .......... ..........  8% 16.8M 13s
 23800K .......... .......... .......... .......... ..........  8% 15.7M 13s
 23850K .......... .......... .......... .......... ..........  8% 19.1M 13s
 23900K .......... .......... .......... .......... ..........  9% 18.6M 13s
 23950K .......... .......... .......... .......... ..........  9% 16.2M 13s
 24000K .......... .......... .......... .......... ..........  9% 19.3M 13s
 24050K .......... .......... .......... .......... ..........  9% 16.1M 13s
 24100K .......... .......... .......... .......... ..........  9% 14.3M 13s
 24150K .......... .......... .......... .......... ..........  9% 24.9M 13s
 24200K .......... .......... .......... .......... ..........  9% 14.6M 13s
 24250K .......... .......... .......... .......... ..........  9% 17.6M 13s
 24300K .......... .......... .......... .......... ..........  9% 15.3M 13s
 24350K .......... .......... .......... .......... ..........  9% 14.5M 13s
 24400K .......... .......... .......... .......... ..........  9% 16.6M 13s
 24450K .......... .......... .......... .......... ..........  9% 15.3M 13s
 24500K .......... .......... .......... .......... ..........  9% 21.5M 13s
 24550K .......... .......... .......... .......... ..........  9% 17.1M 13s
 24600K .......... .......... .......... .......... ..........  9% 21.8M 13s
 24650K .......... .......... .......... .......... ..........  9% 31.5M 13s
 24700K .......... .......... .......... .......... ..........  9% 11.1M 13s
 24750K .......... .......... .......... .......... ..........  9% 24.5M 13s
 24800K .......... .......... .......... .......... ..........  9% 24.5M 13s
 24850K .......... .......... .......... .......... ..........  9% 15.4M 13s
 24900K .......... .......... .......... .......... ..........  9% 18.1M 13s
 24950K .......... .......... .......... .......... ..........  9% 18.0M 13s
 25000K .......... .......... .......... .......... ..........  9% 12.0M 13s
 25050K .......... .......... .......... .......... ..........  9% 43.7M 13s
 25100K .......... .......... .......... .......... ..........  9% 17.1M 13s
 25150K .......... .......... .......... .......... ..........  9% 16.0M 13s
 25200K .......... .......... .......... .......... ..........  9% 16.6M 13s
 25250K .......... .......... .......... .......... ..........  9% 18.9M 13s
 25300K .......... .......... .......... .......... ..........  9% 28.8M 13s
 25350K .......... .......... .......... .......... ..........  9% 15.2M 13s
 25400K .......... .......... .......... .......... ..........  9% 19.6M 13s
 25450K .......... .......... .......... .......... ..........  9% 15.3M 13s
 25500K .......... .......... .......... .......... ..........  9% 17.7M 13s
 25550K .......... .......... .......... .......... ..........  9% 40.1M 13s
 25600K .......... .......... .......... .......... ..........  9% 13.9M 13s
 25650K .......... .......... .......... .......... ..........  9% 33.2M 13s
 25700K .......... .......... .......... .......... ..........  9% 12.5M 13s
 25750K .......... .......... .......... .......... ..........  9% 40.5M 13s
 25800K .......... .......... .......... .......... ..........  9% 15.5M 13s
 25850K .......... .......... .......... .......... ..........  9% 19.8M 13s
 25900K .......... .......... .......... .......... ..........  9% 18.6M 13s
 25950K .......... .......... .......... .......... ..........  9% 17.6M 13s
 26000K .......... .......... .......... .......... ..........  9% 28.9M 13s
 26050K .......... .......... .......... .......... ..........  9% 13.8M 13s
 26100K .......... .......... .......... .......... ..........  9% 17.9M 13s
 26150K .......... .......... .......... .......... ..........  9% 23.9M 13s
 26200K .......... .......... .......... .......... ..........  9% 5.83M 13s
 26250K .......... .......... .......... .......... ..........  9% 58.4M 13s
 26300K .......... .......... .......... .......... ..........  9% 76.8M 13s
 26350K .......... .......... .......... .......... ..........  9% 22.3M 13s
 26400K .......... .......... .......... .......... ..........  9% 16.1M 13s
 26450K .......... .......... .......... .......... ..........  9% 21.2M 13s
 26500K .......... .......... .......... .......... ..........  9% 9.15M 13s
 26550K .......... .......... .......... .......... .......... 10% 28.6M 13s
 26600K .......... .......... .......... .......... .......... 10% 21.3M 13s
 26650K .......... .......... .......... .......... .......... 10% 18.6M 13s
 26700K .......... .......... .......... .......... .......... 10% 17.6M 13s
 26750K .......... .......... .......... .......... .......... 10% 19.3M 13s
 26800K .......... .......... .......... .......... .......... 10% 16.4M 13s
 26850K .......... .......... .......... .......... .......... 10% 16.4M 13s
 26900K .......... .......... .......... .......... .......... 10% 24.7M 13s
 26950K .......... .......... .......... .......... .......... 10% 14.5M 13s
 27000K .......... .......... .......... .......... .......... 10% 18.8M 13s
 27050K .......... .......... .......... .......... .......... 10% 14.8M 13s
 27100K .......... .......... .......... .......... .......... 10% 18.5M 13s
 27150K .......... .......... .......... .......... .......... 10% 23.9M 13s
 27200K .......... .......... .......... .......... .......... 10% 14.5M 13s
 27250K .......... .......... .......... .......... .......... 10% 22.9M 13s
 27300K .......... .......... .......... .......... .......... 10% 19.7M 13s
 27350K .......... .......... .......... .......... .......... 10% 13.0M 13s
 27400K .......... .......... .......... .......... .......... 10% 39.7M 13s
 27450K .......... .......... .......... .......... .......... 10% 16.3M 13s
 27500K .......... .......... .......... .......... .......... 10% 19.4M 13s
 27550K .......... .......... .......... .......... .......... 10% 13.7M 13s
 27600K .......... .......... .......... .......... .......... 10% 15.9M 13s
 27650K .......... .......... .......... .......... .......... 10% 15.1M 13s
 27700K .......... .......... .......... .......... .......... 10% 18.0M 13s
 27750K .......... .......... .......... .......... .......... 10% 35.9M 13s
 27800K .......... .......... .......... .......... .......... 10% 15.5M 13s
 27850K .......... .......... .......... .......... .......... 10% 17.9M 13s
 27900K .......... .......... .......... .......... .......... 10% 17.5M 13s
 27950K .......... .......... .......... .......... .......... 10% 22.9M 13s
 28000K .......... .......... .......... .......... .......... 10% 27.0M 13s
 28050K .......... .......... .......... .......... .......... 10% 14.5M 13s
 28100K .......... .......... .......... .......... .......... 10% 20.7M 13s
 28150K .......... .......... .......... .......... .......... 10% 18.2M 13s
 28200K .......... .......... .......... .......... .......... 10% 11.5M 13s
 28250K .......... .......... .......... .......... .......... 10% 48.5M 13s
 28300K .......... .......... .......... .......... .......... 10% 17.1M 13s
 28350K .......... .......... .......... .......... .......... 10% 12.8M 13s
 28400K .......... .......... .......... .......... .......... 10% 67.2M 13s
 28450K .......... .......... .......... .......... .......... 10% 17.8M 13s
 28500K .......... .......... .......... .......... .......... 10% 15.1M 13s
 28550K .......... .......... .......... .......... .......... 10% 16.3M 13s
 28600K .......... .......... .......... .......... .......... 10% 15.4M 13s
 28650K .......... .......... .......... .......... .......... 10% 15.9M 13s
 28700K .......... .......... .......... .......... .......... 10% 11.4M 13s
 28750K .......... .......... .......... .......... .......... 10% 18.4M 13s
 28800K .......... .......... .......... .......... .......... 10% 22.3M 13s
 28850K .......... .......... .......... .......... .......... 10% 18.2M 13s
 28900K .......... .......... .......... .......... .......... 10% 19.7M 13s
 28950K .......... .......... .......... .......... .......... 10% 15.7M 13s
 29000K .......... .......... .......... .......... .......... 10% 17.2M 13s
 29050K .......... .......... .......... .......... .......... 10% 19.8M 13s
 29100K .......... .......... .......... .......... .......... 10% 11.9M 13s
 29150K .......... .......... .......... .......... .......... 10%  172M 13s
 29200K .......... .......... .......... .......... .......... 11% 24.8M 13s
 29250K .......... .......... .......... .......... .......... 11% 23.2M 13s
 29300K .......... .......... .......... .......... .......... 11% 13.1M 13s
 29350K .......... .......... .......... .......... .......... 11% 27.0M 13s
 29400K .......... .......... .......... .......... .......... 11% 31.1M 13s
 29450K .......... .......... .......... .......... .......... 11% 12.1M 13s
 29500K .......... .......... .......... .......... .......... 11% 26.5M 13s
 29550K .......... .......... .......... .......... .......... 11% 13.5M 13s
 29600K .......... .......... .......... .......... .......... 11% 13.8M 13s
 29650K .......... .......... .......... .......... .......... 11% 23.0M 13s
 29700K .......... .......... .......... .......... .......... 11% 17.5M 13s
 29750K .......... .......... .......... .......... .......... 11% 23.0M 13s
 29800K .......... .......... .......... .......... .......... 11% 25.9M 13s
 29850K .......... .......... .......... .......... .......... 11% 19.5M 13s
 29900K .......... .......... .......... .......... .......... 11% 28.2M 13s
 29950K .......... .......... .......... .......... .......... 11% 17.5M 13s
 30000K .......... .......... .......... .......... .......... 11% 28.3M 13s
 30050K .......... .......... .......... .......... .......... 11% 14.2M 13s
 30100K .......... .......... .......... .......... .......... 11%  108M 13s
 30150K .......... .......... .......... .......... .......... 11%  122M 13s
 30200K .......... .......... .......... .......... .......... 11% 47.0M 13s
 30250K .......... .......... .......... .......... .......... 11% 26.7M 13s
 30300K .......... .......... .......... .......... .......... 11% 23.2M 13s
 30350K .......... .......... .......... .......... .......... 11% 26.0M 13s
 30400K .......... .......... .......... .......... .......... 11% 23.1M 13s
 30450K .......... .......... .......... .......... .......... 11% 18.7M 13s
 30500K .......... .......... .......... .......... .......... 11% 20.7M 13s
 30550K .......... .......... .......... .......... .......... 11% 17.1M 13s
 30600K .......... .......... .......... .......... .......... 11% 15.6M 13s
 30650K .......... .......... .......... .......... .......... 11% 32.7M 13s
 30700K .......... .......... .......... .......... .......... 11% 18.2M 13s
 30750K .......... .......... .......... .......... .......... 11% 18.0M 13s
 30800K .......... .......... .......... .......... .......... 11% 25.2M 13s
 30850K .......... .......... .......... .......... .......... 11% 17.7M 13s
 30900K .......... .......... .......... .......... .......... 11% 12.9M 13s
 30950K .......... .......... .......... .......... .......... 11% 16.4M 13s
 31000K .......... .......... .......... .......... .......... 11% 10.2M 13s
 31050K .......... .......... .......... .......... .......... 11% 14.5M 13s
 31100K .......... .......... .......... .......... .......... 11% 11.8M 13s
 31150K .......... .......... .......... .......... .......... 11% 12.1M 13s
 31200K .......... .......... .......... .......... .......... 11% 14.4M 13s
 31250K .......... .......... .......... .......... .......... 11% 11.6M 13s
 31300K .......... .......... .......... .......... .......... 11% 15.1M 13s
 31350K .......... .......... .......... .......... .......... 11% 11.9M 13s
 31400K .......... .......... .......... .......... .......... 11% 12.7M 13s
 31450K .......... .......... .......... .......... .......... 11% 15.5M 13s
 31500K .......... .......... .......... .......... .......... 11% 15.8M 13s
 31550K .......... .......... .......... .......... .......... 11% 24.9M 13s
 31600K .......... .......... .......... .......... .......... 11% 18.2M 13s
 31650K .......... .......... .......... .......... .......... 11% 30.2M 13s
 31700K .......... .......... .......... .......... .......... 11% 20.5M 13s
 31750K .......... .......... .......... .......... .......... 11% 19.5M 13s
 31800K .......... .......... .......... .......... .......... 11% 14.2M 13s
 31850K .......... .......... .......... .......... .......... 12% 14.4M 13s
 31900K .......... .......... .......... .......... .......... 12% 16.3M 13s
 31950K .......... .......... .......... .......... .......... 12% 11.9M 13s
 32000K .......... .......... .......... .......... .......... 12% 16.7M 13s
 32050K .......... .......... .......... .......... .......... 12% 15.4M 13s
 32100K .......... .......... .......... .......... .......... 12% 13.0M 13s
 32150K .......... .......... .......... .......... .......... 12% 19.5M 13s
 32200K .......... .......... .......... .......... .......... 12% 22.1M 13s
 32250K .......... .......... .......... .......... .......... 12% 20.8M 13s
 32300K .......... .......... .......... .......... .......... 12% 16.6M 13s
 32350K .......... .......... .......... .......... .......... 12% 10.3M 13s
 32400K .......... .......... .......... .......... .......... 12% 70.9M 13s
 32450K .......... .......... .......... .......... .......... 12% 14.9M 13s
 32500K .......... .......... .......... .......... .......... 12% 17.4M 13s
 32550K .......... .......... .......... .......... .......... 12% 14.4M 13s
 32600K .......... .......... .......... .......... .......... 12% 17.4M 13s
 32650K .......... .......... .......... .......... .......... 12% 19.6M 13s
 32700K .......... .......... .......... .......... .......... 12% 12.7M 13s
 32750K .......... .......... .......... .......... .......... 12% 15.2M 13s
 32800K .......... .......... .......... .......... .......... 12% 12.4M 13s
 32850K .......... .......... .......... .......... .......... 12% 24.7M 13s
 32900K .......... .......... .......... .......... .......... 12% 10.7M 13s
 32950K .......... .......... .......... .......... .......... 12% 14.8M 13s
 33000K .......... .......... .......... .......... .......... 12% 21.2M 13s
 33050K .......... .......... .......... .......... .......... 12% 17.4M 13s
 33100K .......... .......... .......... .......... .......... 12% 15.4M 13s
 33150K .......... .......... .......... .......... .......... 12% 16.7M 13s
 33200K .......... .......... .......... .......... .......... 12% 11.4M 13s
 33250K .......... .......... .......... .......... .......... 12% 20.7M 13s
 33300K .......... .......... .......... .......... .......... 12% 16.3M 13s
 33350K .......... .......... .......... .......... .......... 12% 17.6M 13s
 33400K .......... .......... .......... .......... .......... 12% 15.4M 13s
 33450K .......... .......... .......... .......... .......... 12% 15.6M 13s
 33500K .......... .......... .......... .......... .......... 12% 24.5M 13s
 33550K .......... .......... .......... .......... .......... 12% 13.7M 13s
 33600K .......... .......... .......... .......... .......... 12% 15.1M 13s
 33650K .......... .......... .......... .......... .......... 12% 13.6M 13s
 33700K .......... .......... .......... .......... .......... 12% 26.6M 13s
 33750K .......... .......... .......... .......... .......... 12% 19.1M 13s
 33800K .......... .......... .......... .......... .......... 12% 20.2M 13s
 33850K .......... .......... .......... .......... .......... 12% 11.4M 13s
 33900K .......... .......... .......... .......... .......... 12% 17.9M 13s
 33950K .......... .......... .......... .......... .......... 12% 18.9M 13s
 34000K .......... .......... .......... .......... .......... 12% 13.5M 13s
 34050K .......... .......... .......... .......... .......... 12% 23.2M 13s
 34100K .......... .......... .......... .......... .......... 12% 14.3M 13s
 34150K .......... .......... .......... .......... .......... 12% 18.5M 13s
 34200K .......... .......... .......... .......... .......... 12% 13.1M 13s
 34250K .......... .......... .......... .......... .......... 12% 21.0M 13s
 34300K .......... .......... .......... .......... .......... 12% 17.9M 13s
 34350K .......... .......... .......... .......... .......... 12% 12.9M 13s
 34400K .......... .......... .......... .......... .......... 12% 15.8M 13s
 34450K .......... .......... .......... .......... .......... 12% 14.9M 13s
 34500K .......... .......... .......... .......... .......... 12% 17.0M 13s
 34550K .......... .......... .......... .......... .......... 13% 23.8M 13s
 34600K .......... .......... .......... .......... .......... 13% 15.6M 13s
 34650K .......... .......... .......... .......... .......... 13% 18.3M 13s
 34700K .......... .......... .......... .......... .......... 13% 11.9M 13s
 34750K .......... .......... .......... .......... .......... 13% 25.6M 13s
 34800K .......... .......... .......... .......... .......... 13% 16.2M 13s
 34850K .......... .......... .......... .......... .......... 13% 12.1M 13s
 34900K .......... .......... .......... .......... .......... 13% 15.4M 13s
 34950K .......... .......... .......... .......... .......... 13% 24.5M 13s
 35000K .......... .......... .......... .......... .......... 13% 10.3M 13s
 35050K .......... .......... .......... .......... .......... 13% 21.5M 13s
 35100K .......... .......... .......... .......... .......... 13% 13.4M 13s
 35150K .......... .......... .......... .......... .......... 13% 13.4M 13s
 35200K .......... .......... .......... .......... .......... 13% 17.5M 13s
 35250K .......... .......... .......... .......... .......... 13% 19.0M 13s
 35300K .......... .......... .......... .......... .......... 13% 23.3M 13s
 35350K .......... .......... .......... .......... .......... 13% 9.19M 13s
 35400K .......... .......... .......... .......... .......... 13% 18.9M 13s
 35450K .......... .......... .......... .......... .......... 13% 16.9M 13s
 35500K .......... .......... .......... .......... .......... 13% 15.9M 13s
 35550K .......... .......... .......... .......... .......... 13% 11.8M 13s
 35600K .......... .......... .......... .......... .......... 13% 31.6M 13s
 35650K .......... .......... .......... .......... .......... 13% 18.4M 13s
 35700K .......... .......... .......... .......... .......... 13% 9.81M 13s
 35750K .......... .......... .......... .......... .......... 13% 17.8M 13s
 35800K .......... .......... .......... .......... .......... 13% 14.8M 13s
 35850K .......... .......... .......... .......... .......... 13% 12.0M 13s
 35900K .......... .......... .......... .......... .......... 13% 19.3M 13s
 35950K .......... .......... .......... .......... .......... 13% 12.0M 13s
 36000K .......... .......... .......... .......... .......... 13% 12.2M 13s
 36050K .......... .......... .......... .......... .......... 13% 16.0M 13s
 36100K .......... .......... .......... .......... .......... 13% 13.3M 13s
 36150K .......... .......... .......... .......... .......... 13% 13.7M 13s
 36200K .......... .......... .......... .......... .......... 13% 30.1M 13s
 36250K .......... .......... .......... .......... .......... 13% 13.9M 13s
 36300K .......... .......... .......... .......... .......... 13% 11.8M 13s
 36350K .......... .......... .......... .......... .......... 13% 21.7M 13s
 36400K .......... .......... .......... .......... .......... 13% 23.1M 13s
 36450K .......... .......... .......... .......... .......... 13% 11.3M 13s
 36500K .......... .......... .......... .......... .......... 13% 21.8M 13s
 36550K .......... .......... .......... .......... .......... 13% 12.0M 13s
 36600K .......... .......... .......... .......... .......... 13% 13.1M 13s
 36650K .......... .......... .......... .......... .......... 13% 23.1M 13s
 36700K .......... .......... .......... .......... .......... 13% 11.6M 13s
 36750K .......... .......... .......... .......... .......... 13% 17.5M 13s
 36800K .......... .......... .......... .......... .......... 13% 16.0M 13s
 36850K .......... .......... .......... .......... .......... 13% 7.90M 13s
 36900K .......... .......... .......... .......... .......... 13% 45.7M 13s
 36950K .......... .......... .......... .......... .......... 13% 8.79M 13s
 37000K .......... .......... .......... .......... .......... 13% 22.7M 13s
 37050K .......... .......... .......... .......... .......... 13% 8.62M 13s
 37100K .......... .......... .......... .......... .......... 13% 11.9M 13s
 37150K .......... .......... .......... .......... .......... 13% 13.1M 13s
 37200K .......... .......... .......... .......... .......... 14% 15.3M 13s
 37250K .......... .......... .......... .......... .......... 14% 19.3M 13s
 37300K .......... .......... .......... .......... .......... 14% 18.4M 13s
 37350K .......... .......... .......... .......... .......... 14% 10.7M 13s
 37400K .......... .......... .......... .......... .......... 14% 22.0M 13s
 37450K .......... .......... .......... .......... .......... 14% 13.7M 13s
 37500K .......... .......... .......... .......... .......... 14% 13.9M 13s
 37550K .......... .......... .......... .......... .......... 14% 15.4M 13s
 37600K .......... .......... .......... .......... .......... 14% 23.2M 13s
 37650K .......... .......... .......... .......... .......... 14% 18.2M 13s
 37700K .......... .......... .......... .......... .......... 14% 10.4M 13s
 37750K .......... .......... .......... .......... .......... 14% 18.2M 13s
 37800K .......... .......... .......... .......... .......... 14% 15.2M 13s
 37850K .......... .......... .......... .......... .......... 14% 28.4M 13s
 37900K .......... .......... .......... .......... .......... 14% 11.2M 13s
 37950K .......... .......... .......... .......... .......... 14% 16.2M 13s
 38000K .......... .......... .......... .......... .......... 14% 14.4M 13s
 38050K .......... .......... .......... .......... .......... 14% 17.4M 13s
 38100K .......... .......... .......... .......... .......... 14% 9.00M 13s
 38150K .......... .......... .......... .......... .......... 14% 13.4M 13s
 38200K .......... .......... .......... .......... .......... 14% 15.6M 13s
 38250K .......... .......... .......... .......... .......... 14% 20.5M 13s
 38300K .......... .......... .......... .......... .......... 14% 13.9M 13s
 38350K .......... .......... .......... .......... .......... 14% 12.5M 13s
 38400K .......... .......... .......... .......... .......... 14% 12.7M 13s
 38450K .......... .......... .......... .......... .......... 14% 8.44M 13s
 38500K .......... .......... .......... .......... .......... 14% 22.3M 13s
 38550K .......... .......... .......... .......... .......... 14% 13.9M 13s
 38600K .......... .......... .......... .......... .......... 14% 10.9M 13s
 38650K .......... .......... .......... .......... .......... 14% 15.3M 13s
 38700K .......... .......... .......... .......... .......... 14% 9.57M 13s
 38750K .......... .......... .......... .......... .......... 14% 16.0M 13s
 38800K .......... .......... .......... .......... .......... 14% 14.2M 13s
 38850K .......... .......... .......... .......... .......... 14% 8.27M 13s
 38900K .......... .......... .......... .......... .......... 14% 35.6M 13s
 38950K .......... .......... .......... .......... .......... 14% 11.2M 13s
 39000K .......... .......... .......... .......... .......... 14% 18.1M 13s
 39050K .......... .......... .......... .......... .......... 14% 11.5M 13s
 39100K .......... .......... .......... .......... .......... 14% 9.96M 13s
 39150K .......... .......... .......... .......... .......... 14% 15.2M 13s
 39200K .......... .......... .......... .......... .......... 14% 7.63M 13s
 39250K .......... .......... .......... .......... .......... 14% 11.0M 13s
 39300K .......... .......... .......... .......... .......... 14% 16.3M 13s
 39350K .......... .......... .......... .......... .......... 14% 9.28M 13s
 39400K .......... .......... .......... .......... .......... 14% 12.8M 13s
 39450K .......... .......... .......... .......... .......... 14% 12.8M 13s
 39500K .......... .......... .......... .......... .......... 14% 13.8M 13s
 39550K .......... .......... .......... .......... .......... 14% 10.5M 13s
 39600K .......... .......... .......... .......... .......... 14% 15.4M 13s
 39650K .......... .......... .......... .......... .......... 14% 8.51M 13s
 39700K .......... .......... .......... .......... .......... 14% 13.4M 13s
 39750K .......... .......... .......... .......... .......... 14% 15.4M 13s
 39800K .......... .......... .......... .......... .......... 14% 39.2M 13s
 39850K .......... .......... .......... .......... .......... 15% 8.43M 13s
 39900K .......... .......... .......... .......... .......... 15% 15.9M 13s
 39950K .......... .......... .......... .......... .......... 15% 12.2M 13s
 40000K .......... .......... .......... .......... .......... 15% 15.0M 13s
 40050K .......... .......... .......... .......... .......... 15% 15.2M 13s
 40100K .......... .......... .......... .......... .......... 15% 14.3M 13s
 40150K .......... .......... .......... .......... .......... 15% 15.1M 13s
 40200K .......... .......... .......... .......... .......... 15% 16.2M 13s
 40250K .......... .......... .......... .......... .......... 15% 14.3M 13s
 40300K .......... .......... .......... .......... .......... 15% 14.2M 13s
 40350K .......... .......... .......... .......... .......... 15% 14.4M 13s
 40400K .......... .......... .......... .......... .......... 15% 13.2M 13s
 40450K .......... .......... .......... .......... .......... 15% 15.5M 13s
 40500K .......... .......... .......... .......... .......... 15% 10.0M 13s
 40550K .......... .......... .......... .......... .......... 15% 16.2M 13s
 40600K .......... .......... .......... .......... .......... 15% 11.9M 13s
 40650K .......... .......... .......... .......... .......... 15% 16.4M 13s
 40700K .......... .......... .......... .......... .......... 15% 12.2M 13s
 40750K .......... .......... .......... .......... .......... 15% 13.8M 13s
 40800K .......... .......... .......... .......... .......... 15% 13.2M 13s
 40850K .......... .......... .......... .......... .......... 15% 13.4M 13s
 40900K .......... .......... .......... .......... .......... 15% 18.6M 13s
 40950K .......... .......... .......... .......... .......... 15% 18.8M 13s
 41000K .......... .......... .......... .......... .......... 15% 13.3M 13s
 41050K .......... .......... .......... .......... .......... 15% 9.79M 13s
 41100K .......... .......... .......... .......... .......... 15% 18.0M 13s
 41150K .......... .......... .......... .......... .......... 15% 11.6M 13s
 41200K .......... .......... .......... .......... .......... 15% 8.66M 13s
 41250K .......... .......... .......... .......... .......... 15% 14.2M 13s
 41300K .......... .......... .......... .......... .......... 15% 13.1M 13s
 41350K .......... .......... .......... .......... .......... 15% 15.8M 13s
 41400K .......... .......... .......... .......... .......... 15% 16.8M 13s
 41450K .......... .......... .......... .......... .......... 15% 13.2M 13s
 41500K .......... .......... .......... .......... .......... 15% 15.9M 13s
 41550K .......... .......... .......... .......... .......... 15% 17.9M 13s
 41600K .......... .......... .......... .......... .......... 15% 12.0M 13s
 41650K .......... .......... .......... .......... .......... 15% 14.4M 13s
 41700K .......... .......... .......... .......... .......... 15% 17.4M 13s
 41750K .......... .......... .......... .......... .......... 15% 13.7M 13s
 41800K .......... .......... .......... .......... .......... 15% 21.5M 13s
 41850K .......... .......... .......... .......... .......... 15% 13.3M 13s
 41900K .......... .......... .......... .......... .......... 15% 12.2M 13s
 41950K .......... .......... .......... .......... .......... 15% 17.4M 13s
 42000K .......... .......... .......... .......... .......... 15% 11.1M 13s
 42050K .......... .......... .......... .......... .......... 15% 16.0M 13s
 42100K .......... .......... .......... .......... .......... 15% 12.1M 13s
 42150K .......... .......... .......... .......... .......... 15% 15.1M 13s
 42200K .......... .......... .......... .......... .......... 15% 22.7M 13s
 42250K .......... .......... .......... .......... .......... 15% 12.8M 13s
 42300K .......... .......... .......... .......... .......... 15% 12.0M 13s
 42350K .......... .......... .......... .......... .......... 15% 12.2M 13s
 42400K .......... .......... .......... .......... .......... 15% 15.2M 13s
 42450K .......... .......... .......... .......... .......... 15% 12.6M 13s
 42500K .......... .......... .......... .......... .......... 16% 16.0M 13s
 42550K .......... .......... .......... .......... .......... 16% 11.5M 13s
 42600K .......... .......... .......... .......... .......... 16% 12.4M 13s
 42650K .......... .......... .......... .......... .......... 16% 12.4M 13s
 42700K .......... .......... .......... .......... .......... 16% 10.7M 13s
 42750K .......... .......... .......... .......... .......... 16% 16.5M 13s
 42800K .......... .......... .......... .......... .......... 16% 13.6M 13s
 42850K .......... .......... .......... .......... .......... 16% 11.2M 13s
 42900K .......... .......... .......... .......... .......... 16% 14.8M 13s
 42950K .......... .......... .......... .......... .......... 16% 9.71M 13s
 43000K .......... .......... .......... .......... .......... 16% 18.7M 13s
 43050K .......... .......... .......... .......... .......... 16% 20.2M 13s
 43100K .......... .......... .......... .......... .......... 16% 9.21M 13s
 43150K .......... .......... .......... .......... .......... 16% 20.2M 13s
 43200K .......... .......... .......... .......... .......... 16% 11.8M 13s
 43250K .......... .......... .......... .......... .......... 16% 17.6M 13s
 43300K .......... .......... .......... .......... .......... 16% 15.6M 13s
 43350K .......... .......... .......... .......... .......... 16% 11.4M 13s
 43400K .......... .......... .......... .......... .......... 16% 16.7M 13s
 43450K .......... .......... .......... .......... .......... 16% 13.7M 13s
 43500K .......... .......... .......... .......... .......... 16% 17.1M 13s
 43550K .......... .......... .......... .......... .......... 16% 13.1M 13s
 43600K .......... .......... .......... .......... .......... 16% 13.6M 13s
 43650K .......... .......... .......... .......... .......... 16% 12.6M 13s
 43700K .......... .......... .......... .......... .......... 16% 15.9M 13s
 43750K .......... .......... .......... .......... .......... 16% 15.2M 13s
 43800K .......... .......... .......... .......... .......... 16% 12.4M 13s
 43850K .......... .......... .......... .......... .......... 16% 16.1M 13s
 43900K .......... .......... .......... .......... .......... 16% 17.0M 13s
 43950K .......... .......... .......... .......... .......... 16% 11.0M 13s
 44000K .......... .......... .......... .......... .......... 16% 16.5M 13s
 44050K .......... .......... .......... .......... .......... 16% 16.4M 13s
 44100K .......... .......... .......... .......... .......... 16% 11.0M 13s
 44150K .......... .......... .......... .......... .......... 16% 17.7M 13s
 44200K .......... .......... .......... .......... .......... 16% 13.0M 13s
 44250K .......... .......... .......... .......... .......... 16% 12.4M 13s
 44300K .......... .......... .......... .......... .......... 16% 20.0M 13s
 44350K .......... .......... .......... .......... .......... 16% 11.0M 13s
 44400K .......... .......... .......... .......... .......... 16% 17.1M 13s
 44450K .......... .......... .......... .......... .......... 16% 10.7M 13s
 44500K .......... .......... .......... .......... .......... 16% 14.6M 13s
 44550K .......... .......... .......... .......... .......... 16% 13.1M 13s
 44600K .......... .......... .......... .......... .......... 16% 13.4M 13s
 44650K .......... .......... .......... .......... .......... 16% 17.3M 13s
 44700K .......... .......... .......... .......... .......... 16% 12.0M 13s
 44750K .......... .......... .......... .......... .......... 16% 12.7M 13s
 44800K .......... .......... .......... .......... .......... 16% 15.1M 13s
 44850K .......... .......... .......... .......... .......... 16% 13.1M 13s
 44900K .......... .......... .......... .......... .......... 16% 20.5M 13s
 44950K .......... .......... .......... .......... .......... 16% 12.0M 13s
 45000K .......... .......... .......... .......... .......... 16% 10.5M 13s
 45050K .......... .......... .......... .......... .......... 16% 16.0M 13s
 45100K .......... .......... .......... .......... .......... 16% 13.6M 13s
 45150K .......... .......... .......... .......... .......... 17% 16.2M 13s
 45200K .......... .......... .......... .......... .......... 17% 10.3M 13s
 45250K .......... .......... .......... .......... .......... 17% 17.5M 13s
 45300K .......... .......... .......... .......... .......... 17% 16.5M 13s
 45350K .......... .......... .......... .......... .......... 17% 11.2M 13s
 45400K .......... .......... .......... .......... .......... 17% 12.8M 13s
 45450K .......... .......... .......... .......... .......... 17% 11.8M 13s
 45500K .......... .......... .......... .......... .......... 17% 14.2M 13s
 45550K .......... .......... .......... .......... .......... 17% 18.9M 13s
 45600K .......... .......... .......... .......... .......... 17% 12.4M 13s
 45650K .......... .......... .......... .......... .......... 17% 12.4M 13s
 45700K .......... .......... .......... .......... .......... 17% 11.3M 13s
 45750K .......... .......... .......... .......... .......... 17% 22.4M 13s
 45800K .......... .......... .......... .......... .......... 17% 12.9M 13s
 45850K .......... .......... .......... .......... .......... 17% 10.8M 13s
 45900K .......... .......... .......... .......... .......... 17% 14.8M 13s
 45950K .......... .......... .......... .......... .......... 17% 11.0M 13s
 46000K .......... .......... .......... .......... .......... 17% 16.1M 13s
 46050K .......... .......... .......... .......... .......... 17% 15.5M 13s
 46100K .......... .......... .......... .......... .......... 17% 16.7M 13s
 46150K .......... .......... .......... .......... .......... 17% 10.5M 13s
 46200K .......... .......... .......... .......... .......... 17% 17.3M 13s
 46250K .......... .......... .......... .......... .......... 17% 12.3M 13s
 46300K .......... .......... .......... .......... .......... 17% 15.2M 13s
 46350K .......... .......... .......... .......... .......... 17% 13.3M 13s
 46400K .......... .......... .......... .......... .......... 17% 14.5M 13s
 46450K .......... .......... .......... .......... .......... 17% 10.9M 13s
 46500K .......... .......... .......... .......... .......... 17% 10.0M 13s
 46550K .......... .......... .......... .......... .......... 17% 11.1M 13s
 46600K .......... .......... .......... .......... .......... 17% 15.5M 13s
 46650K .......... .......... .......... .......... .......... 17% 12.0M 13s
 46700K .......... .......... .......... .......... .......... 17% 10.6M 13s
 46750K .......... .......... .......... .......... .......... 17% 19.2M 13s
 46800K .......... .......... .......... .......... .......... 17% 14.8M 13s
 46850K .......... .......... .......... .......... .......... 17% 11.2M 13s
 46900K .......... .......... .......... .......... .......... 17% 16.0M 13s
 46950K .......... .......... .......... .......... .......... 17% 10.5M 13s
 47000K .......... .......... .......... .......... .......... 17% 16.4M 13s
 47050K .......... .......... .......... .......... .......... 17% 15.5M 13s
 47100K .......... .......... .......... .......... .......... 17% 11.2M 13s
 47150K .......... .......... .......... .......... .......... 17% 13.8M 13s
 47200K .......... .......... .......... .......... .......... 17% 10.6M 13s
 47250K .......... .......... .......... .......... .......... 17% 15.2M 13s
 47300K .......... .......... .......... .......... .......... 17% 15.1M 13s
 47350K .......... .......... .......... .......... .......... 17% 14.7M 13s
 47400K .......... .......... .......... .......... .......... 17% 11.6M 13s
 47450K .......... .......... .......... .......... .......... 17% 15.4M 13s
 47500K .......... .......... .......... .......... .......... 17% 12.9M 13s
 47550K .......... .......... .......... .......... .......... 17% 13.4M 13s
 47600K .......... .......... .......... .......... .......... 17% 13.9M 13s
 47650K .......... .......... .......... .......... .......... 17% 11.5M 13s
 47700K .......... .......... .......... .......... .......... 17% 12.8M 13s
 47750K .......... .......... .......... .......... .......... 17% 16.2M 13s
 47800K .......... .......... .......... .......... .......... 18% 11.1M 13s
 47850K .......... .......... .......... .......... .......... 18% 13.3M 13s
 47900K .......... .......... .......... .......... .......... 18% 12.8M 13s
 47950K .......... .......... .......... .......... .......... 18% 12.8M 13s
 48000K .......... .......... .......... .......... .......... 18% 17.4M 13s
 48050K .......... .......... .......... .......... .......... 18% 11.7M 13s
 48100K .......... .......... .......... .......... .......... 18% 11.6M 13s
 48150K .......... .......... .......... .......... .......... 18% 15.4M 13s
 48200K .......... .......... .......... .......... .......... 18% 13.1M 13s
 48250K .......... .......... .......... .......... .......... 18% 15.2M 13s
 48300K .......... .......... .......... .......... .......... 18% 18.4M 13s
 48350K .......... .......... .......... .......... .......... 18% 12.7M 13s
 48400K .......... .......... .......... .......... .......... 18% 18.3M 13s
 48450K .......... .......... .......... .......... .......... 18% 16.0M 13s
 48500K .......... .......... .......... .......... .......... 18% 12.6M 13s
 48550K .......... .......... .......... .......... .......... 18% 17.6M 13s
 48600K .......... .......... .......... .......... .......... 18% 13.5M 13s
 48650K .......... .......... .......... .......... .......... 18% 16.0M 13s
 48700K .......... .......... .......... .......... .......... 18% 12.5M 13s
 48750K .......... .......... .......... .......... .......... 18% 17.5M 13s
 48800K .......... .......... .......... .......... .......... 18% 15.4M 13s
 48850K .......... .......... .......... .......... .......... 18% 12.6M 13s
 48900K .......... .......... .......... .......... .......... 18% 22.2M 13s
 48950K .......... .......... .......... .......... .......... 18% 12.6M 13s
 49000K .......... .......... .......... .......... .......... 18% 13.2M 13s
 49050K .......... .......... .......... .......... .......... 18% 17.0M 13s
 49100K .......... .......... .......... .......... .......... 18% 20.0M 13s
 49150K .......... .......... .......... .......... .......... 18% 12.0M 13s
 49200K .......... .......... .......... .......... .......... 18% 16.4M 13s
 49250K .......... .......... .......... .......... .......... 18% 14.9M 13s
 49300K .......... .......... .......... .......... .......... 18% 12.6M 13s
 49350K .......... .......... .......... .......... .......... 18% 15.7M 13s
 49400K .......... .......... .......... .......... .......... 18% 17.6M 13s
 49450K .......... .......... .......... .......... .......... 18% 13.1M 13s
 49500K .......... .......... .......... .......... .......... 18% 18.3M 13s
 49550K .......... .......... .......... .......... .......... 18% 16.1M 13s
 49600K .......... .......... .......... .......... .......... 18% 14.6M 13s
 49650K .......... .......... .......... .......... .......... 18% 15.1M 13s
 49700K .......... .......... .......... .......... .......... 18% 12.5M 13s
 49750K .......... .......... .......... .......... .......... 18% 14.1M 13s
 49800K .......... .......... .......... .......... .......... 18% 23.3M 13s
 49850K .......... .......... .......... .......... .......... 18% 11.9M 13s
 49900K .......... .......... .......... .......... .......... 18% 18.3M 13s
 49950K .......... .......... .......... .......... .......... 18% 13.6M 13s
 50000K .......... .......... .......... .......... .......... 18% 23.1M 13s
 50050K .......... .......... .......... .......... .......... 18% 24.3M 13s
 50100K .......... .......... .......... .......... .......... 18% 14.3M 13s
 50150K .......... .......... .......... .......... .......... 18% 19.4M 13s
 50200K .......... .......... .......... .......... .......... 18% 17.8M 13s
 50250K .......... .......... .......... .......... .......... 18% 14.7M 13s
 50300K .......... .......... .......... .......... .......... 18% 18.9M 13s
 50350K .......... .......... .......... .......... .......... 18% 20.3M 13s
 50400K .......... .......... .......... .......... .......... 18% 4.24M 13s
 50450K .......... .......... .......... .......... .......... 18% 37.3M 13s
 50500K .......... .......... .......... .......... .......... 19% 81.1M 13s
 50550K .......... .......... .......... .......... .......... 19% 95.5M 13s
 50600K .......... .......... .......... .......... .......... 19%  132M 13s
 50650K .......... .......... .......... .......... .......... 19% 20.5M 13s
 50700K .......... .......... .......... .......... .......... 19% 13.6M 13s
 50750K .......... .......... .......... .......... .......... 19% 16.4M 13s
 50800K .......... .......... .......... .......... .......... 19% 16.2M 13s
 50850K .......... .......... .......... .......... .......... 19% 28.0M 13s
 50900K .......... .......... .......... .......... .......... 19% 12.4M 13s
 50950K .......... .......... .......... .......... .......... 19% 29.8M 13s
 51000K .......... .......... .......... .......... .......... 19% 12.9M 13s
 51050K .......... .......... .......... .......... .......... 19% 37.8M 13s
 51100K .......... .......... .......... .......... .......... 19% 20.4M 13s
 51150K .......... .......... .......... .......... .......... 19% 16.1M 13s
 51200K .......... .......... .......... .......... .......... 19% 20.7M 13s
 51250K .......... .......... .......... .......... .......... 19% 16.6M 13s
 51300K .......... .......... .......... .......... .......... 19% 33.1M 13s
 51350K .......... .......... .......... .......... .......... 19% 13.8M 13s
 51400K .......... .......... .......... .......... .......... 19% 41.6M 13s
 51450K .......... .......... .......... .......... .......... 19% 15.3M 13s
 51500K .......... .......... .......... .......... .......... 19% 60.2M 13s
 51550K .......... .......... .......... .......... .......... 19% 14.1M 13s
 51600K .......... .......... .......... .......... .......... 19% 39.4M 13s
 51650K .......... .......... .......... .......... .......... 19% 14.9M 13s
 51700K .......... .......... .......... .......... .......... 19% 40.9M 13s
 51750K .......... .......... .......... .......... .......... 19% 23.8M 13s
 51800K .......... .......... .......... .......... .......... 19% 22.4M 13s
 51850K .......... .......... .......... .......... .......... 19% 21.5M 13s
 51900K .......... .......... .......... .......... .......... 19% 14.7M 13s
 51950K .......... .......... .......... .......... .......... 19% 33.7M 13s
 52000K .......... .......... .......... .......... .......... 19% 20.8M 13s
 52050K .......... .......... .......... .......... .......... 19% 24.9M 13s
 52100K .......... .......... .......... .......... .......... 19% 17.3M 13s
 52150K .......... .......... .......... .......... .......... 19% 25.8M 13s
 52200K .......... .......... .......... .......... .......... 19% 17.6M 13s
 52250K .......... .......... .......... .......... .......... 19% 15.4M 13s
 52300K .......... .......... .......... .......... .......... 19% 32.0M 13s
 52350K .......... .......... .......... .......... .......... 19% 13.8M 13s
 52400K .......... .......... .......... .......... .......... 19% 85.4M 13s
 52450K .......... .......... .......... .......... .......... 19% 21.7M 13s
 52500K .......... .......... .......... .......... .......... 19% 16.0M 13s
 52550K .......... .......... .......... .......... .......... 19% 32.1M 13s
 52600K .......... .......... .......... .......... .......... 19% 15.8M 13s
 52650K .......... .......... .......... .......... .......... 19% 34.3M 13s
 52700K .......... .......... .......... .......... .......... 19% 14.4M 13s
 52750K .......... .......... .......... .......... .......... 19% 32.3M 13s
 52800K .......... .......... .......... .......... .......... 19% 16.0M 13s
 52850K .......... .......... .......... .......... .......... 19% 26.2M 13s
 52900K .......... .......... .......... .......... .......... 19% 17.8M 13s
 52950K .......... .......... .......... .......... .......... 19% 27.4M 13s
 53000K .......... .......... .......... .......... .......... 19% 78.2M 13s
 53050K .......... .......... .......... .......... .......... 19% 11.3M 13s
 53100K .......... .......... .......... .......... .......... 19% 39.1M 13s
 53150K .......... .......... .......... .......... .......... 20% 16.5M 13s
 53200K .......... .......... .......... .......... .......... 20% 40.4M 13s
 53250K .......... .......... .......... .......... .......... 20% 14.8M 13s
 53300K .......... .......... .......... .......... .......... 20% 35.3M 13s
 53350K .......... .......... .......... .......... .......... 20% 60.0M 13s
 53400K .......... .......... .......... .......... .......... 20% 13.3M 13s
 53450K .......... .......... .......... .......... .......... 20% 35.8M 13s
 53500K .......... .......... .......... .......... .......... 20% 14.4M 13s
 53550K .......... .......... .......... .......... .......... 20% 37.7M 13s
 53600K .......... .......... .......... .......... .......... 20% 46.1M 12s
 53650K .......... .......... .......... .......... .......... 20% 13.8M 12s
 53700K .......... .......... .......... .......... .......... 20% 32.4M 12s
 53750K .......... .......... .......... .......... .......... 20% 15.5M 12s
 53800K .......... .......... .......... .......... .......... 20% 30.0M 12s
 53850K .......... .......... .......... .......... .......... 20% 67.7M 12s
 53900K .......... .......... .......... .......... .......... 20% 12.3M 12s
 53950K .......... .......... .......... .......... .......... 20% 63.1M 12s
 54000K .......... .......... .......... .......... .......... 20% 17.9M 12s
 54050K .......... .......... .......... .......... .......... 20% 18.8M 12s
 54100K .......... .......... .......... .......... .......... 20% 45.2M 12s
 54150K .......... .......... .......... .......... .......... 20% 6.59M 12s
 54200K .......... .......... .......... .......... .......... 20% 62.9M 12s
 54250K .......... .......... .......... .......... .......... 20%  108M 12s
 54300K .......... .......... .......... .......... .......... 20% 43.7M 12s
 54350K .......... .......... .......... .......... .......... 20% 15.3M 12s
 54400K .......... .......... .......... .......... .......... 20% 22.7M 12s
 54450K .......... .......... .......... .......... .......... 20% 11.4M 12s
 54500K .......... .......... .......... .......... .......... 20% 18.7M 12s
 54550K .......... .......... .......... .......... .......... 20% 23.3M 12s
 54600K .......... .......... .......... .......... .......... 20% 12.3M 12s
 54650K .......... .......... .......... .......... .......... 20% 49.4M 12s
 54700K .......... .......... .......... .......... .......... 20% 12.9M 12s
 54750K .......... .......... .......... .......... .......... 20% 91.4M 12s
 54800K .......... .......... .......... .......... .......... 20% 11.8M 12s
 54850K .......... .......... .......... .......... .......... 20% 28.6M 12s
 54900K .......... .......... .......... .......... .......... 20% 26.4M 12s
 54950K .......... .......... .......... .......... .......... 20% 41.3M 12s
 55000K .......... .......... .......... .......... .......... 20% 18.9M 12s
 55050K .......... .......... .......... .......... .......... 20% 74.9M 12s
 55100K .......... .......... .......... .......... .......... 20% 14.1M 12s
 55150K .......... .......... .......... .......... .......... 20% 71.5M 12s
 55200K .......... .......... .......... .......... .......... 20% 17.2M 12s
 55250K .......... .......... .......... .......... .......... 20%  144M 12s
 55300K .......... .......... .......... .......... .......... 20% 15.9M 12s
 55350K .......... .......... .......... .......... .......... 20% 49.5M 12s
 55400K .......... .......... .......... .......... .......... 20% 18.2M 12s
 55450K .......... .......... .......... .......... .......... 20% 15.2M 12s
 55500K .......... .......... .......... .......... .......... 20% 64.8M 12s
 55550K .......... .......... .......... .......... .......... 20% 38.6M 12s
 55600K .......... .......... .......... .......... .......... 20% 22.8M 12s
 55650K .......... .......... .......... .......... .......... 20% 21.1M 12s
 55700K .......... .......... .......... .......... .......... 20% 43.3M 12s
 55750K .......... .......... .......... .......... .......... 20% 14.9M 12s
 55800K .......... .......... .......... .......... .......... 21% 60.7M 12s
 55850K .......... .......... .......... .......... .......... 21% 16.2M 12s
 55900K .......... .......... .......... .......... .......... 21% 45.7M 12s
 55950K .......... .......... .......... .......... .......... 21% 18.0M 12s
 56000K .......... .......... .......... .......... .......... 21% 43.4M 12s
 56050K .......... .......... .......... .......... .......... 21% 17.8M 12s
 56100K .......... .......... .......... .......... .......... 21% 40.9M 12s
 56150K .......... .......... .......... .......... .......... 21% 18.2M 12s
 56200K .......... .......... .......... .......... .......... 21% 70.6M 12s
 56250K .......... .......... .......... .......... .......... 21% 15.3M 12s
 56300K .......... .......... .......... .......... .......... 21% 50.5M 12s
 56350K .......... .......... .......... .......... .......... 21% 16.7M 12s
 56400K .......... .......... .......... .......... .......... 21% 75.2M 12s
 56450K .......... .......... .......... .......... .......... 21% 16.0M 12s
 56500K .......... .......... .......... .......... .......... 21% 29.0M 12s
 56550K .......... .......... .......... .......... .......... 21% 21.0M 12s
 56600K .......... .......... .......... .......... .......... 21% 60.5M 12s
 56650K .......... .......... .......... .......... .......... 21% 18.5M 12s
 56700K .......... .......... .......... .......... .......... 21% 32.3M 12s
 56750K .......... .......... .......... .......... .......... 21% 26.3M 12s
 56800K .......... .......... .......... .......... .......... 21% 48.7M 12s
 56850K .......... .......... .......... .......... .......... 21% 24.9M 12s
 56900K .......... .......... .......... .......... .......... 21% 9.97M 12s
 56950K .......... .......... .......... .......... .......... 21% 37.2M 12s
 57000K .......... .......... .......... .......... .......... 21% 60.2M 12s
 57050K .......... .......... .......... .......... .......... 21%  110M 12s
 57100K .......... .......... .......... .......... .......... 21% 16.3M 12s
 57150K .......... .......... .......... .......... .......... 21% 47.3M 12s
 57200K .......... .......... .......... .......... .......... 21% 26.6M 12s
 57250K .......... .......... .......... .......... .......... 21% 20.0M 12s
 57300K .......... .......... .......... .......... .......... 21% 24.8M 12s
 57350K .......... .......... .......... .......... .......... 21% 26.6M 12s
 57400K .......... .......... .......... .......... .......... 21% 25.4M 12s
 57450K .......... .......... .......... .......... .......... 21% 37.6M 12s
 57500K .......... .......... .......... .......... .......... 21% 11.2M 12s
 57550K .......... .......... .......... .......... .......... 21% 26.9M 12s
 57600K .......... .......... .......... .......... .......... 21%  104M 12s
 57650K .......... .......... .......... .......... .......... 21% 20.2M 12s
 57700K .......... .......... .......... .......... .......... 21% 13.7M 12s
 57750K .......... .......... .......... .......... .......... 21% 36.6M 12s
 57800K .......... .......... .......... .......... .......... 21% 15.0M 12s
 57850K .......... .......... .......... .......... .......... 21% 17.3M 12s
 57900K .......... .......... .......... .......... .......... 21% 22.4M 12s
 57950K .......... .......... .......... .......... .......... 21% 15.2M 12s
 58000K .......... .......... .......... .......... .......... 21% 27.3M 12s
 58050K .......... .......... .......... .......... .......... 21% 19.2M 12s
 58100K .......... .......... .......... .......... .......... 21% 17.0M 12s
 58150K .......... .......... .......... .......... .......... 21% 19.9M 12s
 58200K .......... .......... .......... .......... .......... 21% 17.7M 12s
 58250K .......... .......... .......... .......... .......... 21% 19.9M 12s
 58300K .......... .......... .......... .......... .......... 21% 19.6M 12s
 58350K .......... .......... .......... .......... .......... 21% 17.4M 12s
 58400K .......... .......... .......... .......... .......... 21% 18.6M 12s
 58450K .......... .......... .......... .......... .......... 22% 12.9M 12s
 58500K .......... .......... .......... .......... .......... 22% 8.91M 12s
 58550K .......... .......... .......... .......... .......... 22% 10.2M 12s
 58600K .......... .......... .......... .......... .......... 22% 9.58M 12s
 58650K .......... .......... .......... .......... .......... 22% 14.0M 12s
 58700K .......... .......... .......... .......... .......... 22% 12.4M 12s
 58750K .......... .......... .......... .......... .......... 22% 18.1M 12s
 58800K .......... .......... .......... .......... .......... 22% 11.6M 12s
 58850K .......... .......... .......... .......... .......... 22% 15.7M 12s
 58900K .......... .......... .......... .......... .......... 22% 13.2M 12s
 58950K .......... .......... .......... .......... .......... 22% 18.5M 12s
 59000K .......... .......... .......... .......... .......... 22% 12.2M 12s
 59050K .......... .......... .......... .......... .......... 22% 16.0M 12s
 59100K .......... .......... .......... .......... .......... 22% 14.7M 12s
 59150K .......... .......... .......... .......... .......... 22% 18.6M 12s
 59200K .......... .......... .......... .......... .......... 22% 14.7M 12s
 59250K .......... .......... .......... .......... .......... 22% 16.4M 12s
 59300K .......... .......... .......... .......... .......... 22% 17.8M 12s
 59350K .......... .......... .......... .......... .......... 22% 21.4M 12s
 59400K .......... .......... .......... .......... .......... 22% 17.0M 12s
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 59500K .......... .......... .......... .......... .......... 22% 23.6M 12s
 59550K .......... .......... .......... .......... .......... 22% 12.6M 12s
 59600K .......... .......... .......... .......... .......... 22% 17.6M 12s
 59650K .......... .......... .......... .......... .......... 22% 15.1M 12s
 59700K .......... .......... .......... .......... .......... 22% 13.2M 12s
 59750K .......... .......... .......... .......... .......... 22% 17.8M 12s
 59800K .......... .......... .......... .......... .......... 22% 25.5M 12s
 59850K .......... .......... .......... .......... .......... 22% 13.0M 12s
 59900K .......... .......... .......... .......... .......... 22% 15.9M 12s
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 60000K .......... .......... .......... .......... .......... 22% 15.1M 12s
 60050K .......... .......... .......... .......... .......... 22% 23.4M 12s
 60100K .......... .......... .......... .......... .......... 22% 14.6M 12s
 60150K .......... .......... .......... .......... .......... 22% 16.4M 12s
 60200K .......... .......... .......... .......... .......... 22% 11.7M 12s
 60250K .......... .......... .......... .......... .......... 22% 25.9M 12s
 60300K .......... .......... .......... .......... .......... 22% 18.1M 12s
 60350K .......... .......... .......... .......... .......... 22% 15.6M 12s
 60400K .......... .......... .......... .......... .......... 22% 26.2M 12s
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 60500K .......... .......... .......... .......... .......... 22% 16.9M 12s
 60550K .......... .......... .......... .......... .......... 22% 25.7M 12s
 60600K .......... .......... .......... .......... .......... 22% 11.0M 12s
 60650K .......... .......... .......... .......... .......... 22% 85.7M 12s
 60700K .......... .......... .......... .......... .......... 22% 14.9M 12s
 60750K .......... .......... .......... .......... .......... 22% 17.0M 12s
 60800K .......... .......... .......... .......... .......... 22% 18.8M 12s
 60850K .......... .......... .......... .......... .......... 22% 16.5M 12s
 60900K .......... .......... .......... .......... .......... 22% 24.2M 12s
 60950K .......... .......... .......... .......... .......... 22% 16.3M 12s
 61000K .......... .......... .......... .......... .......... 22% 22.2M 12s
 61050K .......... .......... .......... .......... .......... 22% 19.8M 12s
 61100K .......... .......... .......... .......... .......... 23% 13.4M 12s
 61150K .......... .......... .......... .......... .......... 23% 20.7M 12s
 61200K .......... .......... .......... .......... .......... 23% 22.9M 12s
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 61450K .......... .......... .......... .......... .......... 23% 30.7M 12s
 61500K .......... .......... .......... .......... .......... 23% 16.2M 12s
 61550K .......... .......... .......... .......... .......... 23% 13.3M 12s
 61600K .......... .......... .......... .......... .......... 23% 19.9M 12s
 61650K .......... .......... .......... .......... .......... 23% 32.3M 12s
 61700K .......... .......... .......... .......... .......... 23% 10.6M 12s
 61750K .......... .......... .......... .......... .......... 23% 26.5M 12s
 61800K .......... .......... .......... .......... .......... 23% 13.9M 12s
 61850K .......... .......... .......... .......... .......... 23% 17.6M 12s
 61900K .......... .......... .......... .......... .......... 23% 21.7M 12s
 61950K .......... .......... .......... .......... .......... 23% 13.3M 12s
 62000K .......... .......... .......... .......... .......... 23% 28.6M 12s
 62050K .......... .......... .......... .......... .......... 23% 15.9M 12s
 62100K .......... .......... .......... .......... .......... 23% 14.4M 12s
 62150K .......... .......... .......... .......... .......... 23% 23.6M 12s
 62200K .......... .......... .......... .......... .......... 23% 14.1M 12s
 62250K .......... .......... .......... .......... .......... 23% 32.9M 12s
 62300K .......... .......... .......... .......... .......... 23% 22.7M 12s
 62350K .......... .......... .......... .......... .......... 23% 14.5M 12s
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 62500K .......... .......... .......... .......... .......... 23% 16.1M 12s
 62550K .......... .......... .......... .......... .......... 23% 17.9M 12s
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 62650K .......... .......... .......... .......... .......... 23% 49.4M 12s
 62700K .......... .......... .......... .......... .......... 23% 16.4M 12s
 62750K .......... .......... .......... .......... .......... 23% 13.4M 12s
 62800K .......... .......... .......... .......... .......... 23% 47.8M 12s
 62850K .......... .......... .......... .......... .......... 23% 15.2M 12s
 62900K .......... .......... .......... .......... .......... 23% 14.8M 12s
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 63000K .......... .......... .......... .......... .......... 23% 23.7M 12s
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 63100K .......... .......... .......... .......... .......... 23% 14.6M 12s
 63150K .......... .......... .......... .......... .......... 23% 19.3M 12s
 63200K .......... .......... .......... .......... .......... 23% 21.3M 12s
 63250K .......... .......... .......... .......... .......... 23% 22.2M 12s
 63300K .......... .......... .......... .......... .......... 23% 18.9M 12s
 63350K .......... .......... .......... .......... .......... 23% 20.4M 12s
 63400K .......... .......... .......... .......... .......... 23% 17.1M 12s
 63450K .......... .......... .......... .......... .......... 23% 14.1M 12s
 63500K .......... .......... .......... .......... .......... 23% 22.4M 12s
 63550K .......... .......... .......... .......... .......... 23% 25.8M 12s
 63600K .......... .......... .......... .......... .......... 23% 13.5M 12s
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 63700K .......... .......... .......... .......... .......... 23% 11.1M 12s
 63750K .......... .......... .......... .......... .......... 24% 21.6M 12s
 63800K .......... .......... .......... .......... .......... 24% 18.9M 12s
 63850K .......... .......... .......... .......... .......... 24% 14.7M 12s
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 63950K .......... .......... .......... .......... .......... 24% 11.4M 12s
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 64100K .......... .......... .......... .......... .......... 24% 17.3M 12s
 64150K .......... .......... .......... .......... .......... 24% 12.1M 12s
 64200K .......... .......... .......... .......... .......... 24% 22.2M 12s
 64250K .......... .......... .......... .......... .......... 24% 15.0M 12s
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 64400K .......... .......... .......... .......... .......... 24% 11.1M 12s
 64450K .......... .......... .......... .......... .......... 24% 21.7M 12s
 64500K .......... .......... .......... .......... .......... 24% 13.6M 12s
 64550K .......... .......... .......... .......... .......... 24% 25.6M 12s
 64600K .......... .......... .......... .......... .......... 24% 16.0M 12s
 64650K .......... .......... .......... .......... .......... 24% 22.0M 12s
 64700K .......... .......... .......... .......... .......... 24% 12.2M 12s
 64750K .......... .......... .......... .......... .......... 24% 17.2M 12s
 64800K .......... .......... .......... .......... .......... 24% 15.9M 12s
 64850K .......... .......... .......... .......... .......... 24% 14.0M 12s
 64900K .......... .......... .......... .......... .......... 24% 16.9M 12s
 64950K .......... .......... .......... .......... .......... 24% 20.8M 12s
 65000K .......... .......... .......... .......... .......... 24% 11.7M 12s
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 65100K .......... .......... .......... .......... .......... 24% 10.3M 12s
 65150K .......... .......... .......... .......... .......... 24% 19.6M 12s
 65200K .......... .......... .......... .......... .......... 24% 12.8M 12s
 65250K .......... .......... .......... .......... .......... 24% 14.0M 12s
 65300K .......... .......... .......... .......... .......... 24% 16.5M 12s
 65350K .......... .......... .......... .......... .......... 24% 12.1M 12s
 65400K .......... .......... .......... .......... .......... 24% 15.9M 12s
 65450K .......... .......... .......... .......... .......... 24% 22.3M 12s
 65500K .......... .......... .......... .......... .......... 24% 12.5M 12s
 65550K .......... .......... .......... .......... .......... 24% 21.3M 12s
 65600K .......... .......... .......... .......... .......... 24% 16.6M 12s
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 65700K .......... .......... .......... .......... .......... 24% 13.4M 12s
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 65800K .......... .......... .......... .......... .......... 24% 13.5M 12s
 65850K .......... .......... .......... .......... .......... 24% 18.7M 12s
 65900K .......... .......... .......... .......... .......... 24% 13.3M 12s
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 66000K .......... .......... .......... .......... .......... 24% 17.8M 12s
 66050K .......... .......... .......... .......... .......... 24% 19.7M 12s
 66100K .......... .......... .......... .......... .......... 24% 11.6M 12s
 66150K .......... .......... .......... .......... .......... 24% 25.4M 12s
 66200K .......... .......... .......... .......... .......... 24% 12.6M 12s
 66250K .......... .......... .......... .......... .......... 24% 20.1M 12s
 66300K .......... .......... .......... .......... .......... 24% 18.5M 12s
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 66450K .......... .......... .......... .......... .......... 25% 14.7M 12s
 66500K .......... .......... .......... .......... .......... 25% 20.0M 12s
 66550K .......... .......... .......... .......... .......... 25% 23.1M 12s
 66600K .......... .......... .......... .......... .......... 25% 18.7M 12s
 66650K .......... .......... .......... .......... .......... 25% 12.8M 12s
 66700K .......... .......... .......... .......... .......... 25% 16.4M 12s
 66750K .......... .......... .......... .......... .......... 25% 13.7M 12s
 66800K .......... .......... .......... .......... .......... 25% 19.6M 12s
 66850K .......... .......... .......... .......... .......... 25% 21.0M 12s
 66900K .......... .......... .......... .......... .......... 25% 12.2M 12s
 66950K .......... .......... .......... .......... .......... 25% 16.9M 11s
 67000K .......... .......... .......... .......... .......... 25% 16.6M 11s
 67050K .......... .......... .......... .......... .......... 25% 14.9M 11s
 67100K .......... .......... .......... .......... .......... 25% 21.5M 11s
 67150K .......... .......... .......... .......... .......... 25% 18.2M 11s
 67200K .......... .......... .......... .......... .......... 25% 12.3M 11s
 67250K .......... .......... .......... .......... .......... 25% 18.0M 11s
 67300K .......... .......... .......... .......... .......... 25% 15.0M 11s
 67350K .......... .......... .......... .......... .......... 25% 17.4M 11s
 67400K .......... .......... .......... .......... .......... 25% 14.0M 11s
 67450K .......... .......... .......... .......... .......... 25% 14.1M 11s
 67500K .......... .......... .......... .......... .......... 25% 15.4M 11s
 67550K .......... .......... .......... .......... .......... 25% 16.1M 11s
 67600K .......... .......... .......... .......... .......... 25% 14.2M 11s
 67650K .......... .......... .......... .......... .......... 25% 19.4M 11s
 67700K .......... .......... .......... .......... .......... 25% 11.6M 11s
 67750K .......... .......... .......... .......... .......... 25% 14.0M 11s
 67800K .......... .......... .......... .......... .......... 25% 23.5M 11s
 67850K .......... .......... .......... .......... .......... 25% 20.4M 11s
 67900K .......... .......... .......... .......... .......... 25% 32.3M 11s
 67950K .......... .......... .......... .......... .......... 25% 17.2M 11s
 68000K .......... .......... .......... .......... .......... 25% 33.3M 11s
 68050K .......... .......... .......... .......... .......... 25% 21.1M 11s
 68100K .......... .......... .......... .......... .......... 25% 25.1M 11s
 68150K .......... .......... .......... .......... .......... 25% 18.5M 11s
 68200K .......... .......... .......... .......... .......... 25% 30.7M 11s
 68250K .......... .......... .......... .......... .......... 25% 19.6M 11s
 68300K .......... .......... .......... .......... .......... 25% 19.6M 11s
 68350K .......... .......... .......... .......... .......... 25% 29.7M 11s
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 69100K .......... .......... .......... .......... .......... 26% 28.6M 11s
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 69250K .......... .......... .......... .......... .......... 26%  120M 11s
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 72150K .......... .......... .......... .......... .......... 27% 20.3M 11s
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 82050K .......... .......... .......... .......... .......... 30% 34.2M 10s
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 82150K .......... .......... .......... .......... .......... 30% 22.5M 10s
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 82450K .......... .......... .......... .......... .......... 31% 11.5M 10s
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 82550K .......... .......... .......... .......... .......... 31% 80.0M 10s
 82600K .......... .......... .......... .......... .......... 31% 22.8M 10s
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 82800K .......... .......... .......... .......... .......... 31% 50.9M 10s
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 96600K .......... .......... .......... .......... .......... 36% 22.4M 9s
 96650K .......... .......... .......... .......... .......... 36% 26.7M 9s
 96700K .......... .......... .......... .......... .......... 36% 25.3M 9s
 96750K .......... .......... .......... .......... .......... 36% 21.8M 9s
 96800K .......... .......... .......... .......... .......... 36% 25.9M 9s
 96850K .......... .......... .......... .......... .......... 36% 13.0M 9s
 96900K .......... .......... .......... .......... .......... 36% 82.2M 9s
 96950K .......... .......... .......... .......... .......... 36% 12.2M 9s
 97000K .......... .......... .......... .......... .......... 36% 45.6M 9s
 97050K .......... .......... .......... .......... .......... 36% 22.4M 9s
 97100K .......... .......... .......... .......... .......... 36% 64.0M 9s
 97150K .......... .......... .......... .......... .......... 36% 20.0M 9s
 97200K .......... .......... .......... .......... .......... 36% 44.8M 9s
 97250K .......... .......... .......... .......... .......... 36% 33.3M 9s
 97300K .......... .......... .......... .......... .......... 36% 21.6M 9s
 97350K .......... .......... .......... .......... .......... 36% 19.5M 9s
 97400K .......... .......... .......... .......... .......... 36% 16.2M 9s
 97450K .......... .......... .......... .......... .......... 36% 51.5M 9s
 97500K .......... .......... .......... .......... .......... 36% 14.8M 9s
 97550K .......... .......... .......... .......... .......... 36% 39.9M 9s
 97600K .......... .......... .......... .......... .......... 36% 22.6M 9s
 97650K .......... .......... .......... .......... .......... 36% 31.2M 9s
 97700K .......... .......... .......... .......... .......... 36% 21.8M 9s
 97750K .......... .......... .......... .......... .......... 36% 28.6M 9s
 97800K .......... .......... .......... .......... .......... 36% 21.6M 9s
 97850K .......... .......... .......... .......... .......... 36% 28.4M 9s
 97900K .......... .......... .......... .......... .......... 36% 52.0M 9s
 97950K .......... .......... .......... .......... .......... 36% 15.1M 9s
 98000K .......... .......... .......... .......... .......... 36% 33.8M 9s
 98050K .......... .......... .......... .......... .......... 36% 20.3M 9s
 98100K .......... .......... .......... .......... .......... 36% 30.5M 9s
 98150K .......... .......... .......... .......... .......... 36% 25.3M 9s
 98200K .......... .......... .......... .......... .......... 36% 23.5M 9s
 98250K .......... .......... .......... .......... .......... 36% 17.2M 9s
 98300K .......... .......... .......... .......... .......... 37% 30.0M 9s
 98350K .......... .......... .......... .......... .......... 37% 13.3M 9s
 98400K .......... .......... .......... .......... .......... 37% 62.8M 9s
 98450K .......... .......... .......... .......... .......... 37% 21.5M 9s
 98500K .......... .......... .......... .......... .......... 37% 38.0M 9s
 98550K .......... .......... .......... .......... .......... 37% 20.1M 9s
 98600K .......... .......... .......... .......... .......... 37% 30.1M 9s
 98650K .......... .......... .......... .......... .......... 37% 17.2M 9s
 98700K .......... .......... .......... .......... .......... 37% 22.5M 9s
 98750K .......... .......... .......... .......... .......... 37% 18.9M 9s
 98800K .......... .......... .......... .......... .......... 37% 34.0M 9s
 98850K .......... .......... .......... .......... .......... 37% 21.9M 9s
 98900K .......... .......... .......... .......... .......... 37% 31.7M 9s
 98950K .......... .......... .......... .......... .......... 37% 15.8M 9s
 99000K .......... .......... .......... .......... .......... 37% 49.2M 9s
 99050K .......... .......... .......... .......... .......... 37% 17.1M 9s
 99100K .......... .......... .......... .......... .......... 37% 46.4M 9s
 99150K .......... .......... .......... .......... .......... 37% 20.4M 9s
 99200K .......... .......... .......... .......... .......... 37% 21.6M 9s
 99250K .......... .......... .......... .......... .......... 37% 22.3M 9s
 99300K .......... .......... .......... .......... .......... 37% 31.9M 9s
 99350K .......... .......... .......... .......... .......... 37% 18.7M 9s
 99400K .......... .......... .......... .......... .......... 37% 19.3M 9s
 99450K .......... .......... .......... .......... .......... 37% 28.7M 9s
 99500K .......... .......... .......... .......... .......... 37% 20.0M 9s
 99550K .......... .......... .......... .......... .......... 37% 25.2M 9s
 99600K .......... .......... .......... .......... .......... 37% 21.3M 9s
 99650K .......... .......... .......... .......... .......... 37% 36.0M 9s
 99700K .......... .......... .......... .......... .......... 37% 24.9M 9s
 99750K .......... .......... .......... .......... .......... 37% 15.1M 9s
 99800K .......... .......... .......... .......... .......... 37% 42.1M 9s
 99850K .......... .......... .......... .......... .......... 37% 32.5M 9s
 99900K .......... .......... .......... .......... .......... 37% 25.5M 9s
 99950K .......... .......... .......... .......... .......... 37% 58.1M 9s
100000K .......... .......... .......... .......... .......... 37% 14.4M 9s
100050K .......... .......... .......... .......... .......... 37% 44.9M 9s
100100K .......... .......... .......... .......... .......... 37% 22.7M 9s
100150K .......... .......... .......... .......... .......... 37% 18.8M 9s
100200K .......... .......... .......... .......... .......... 37% 24.9M 9s
100250K .......... .......... .......... .......... .......... 37% 54.4M 9s
100300K .......... .......... .......... .......... .......... 37% 20.4M 9s
100350K .......... .......... .......... .......... .......... 37% 24.8M 9s
100400K .......... .......... .......... .......... .......... 37% 28.3M 9s
100450K .......... .......... .......... .......... .......... 37% 21.7M 9s
100500K .......... .......... .......... .......... .......... 37% 62.2M 9s
100550K .......... .......... .......... .......... .......... 37% 19.7M 9s
100600K .......... .......... .......... .......... .......... 37% 32.2M 9s
100650K .......... .......... .......... .......... .......... 37% 19.1M 9s
100700K .......... .......... .......... .......... .......... 37% 16.5M 9s
100750K .......... .......... .......... .......... .......... 37%  101M 9s
100800K .......... .......... .......... .......... .......... 37% 17.0M 9s
100850K .......... .......... .......... .......... .......... 37% 37.0M 9s
100900K .......... .......... .......... .......... .......... 37% 23.9M 9s
100950K .......... .......... .......... .......... .......... 37% 20.7M 9s
101000K .......... .......... .......... .......... .......... 38% 85.7M 9s
101050K .......... .......... .......... .......... .......... 38% 14.5M 9s
101100K .......... .......... .......... .......... .......... 38% 61.6M 9s
101150K .......... .......... .......... .......... .......... 38% 16.6M 9s
101200K .......... .......... .......... .......... .......... 38% 22.3M 9s
101250K .......... .......... .......... .......... .......... 38% 92.6M 9s
101300K .......... .......... .......... .......... .......... 38% 14.7M 9s
101350K .......... .......... .......... .......... .......... 38% 37.2M 9s
101400K .......... .......... .......... .......... .......... 38% 27.4M 9s
101450K .......... .......... .......... .......... .......... 38% 16.1M 9s
101500K .......... .......... .......... .......... .......... 38% 49.6M 9s
101550K .......... .......... .......... .......... .......... 38% 17.5M 9s
101600K .......... .......... .......... .......... .......... 38% 38.7M 9s
101650K .......... .......... .......... .......... .......... 38% 84.1M 9s
101700K .......... .......... .......... .......... .......... 38% 18.3M 9s
101750K .......... .......... .......... .......... .......... 38% 54.2M 9s
101800K .......... .......... .......... .......... .......... 38% 24.0M 9s
101850K .......... .......... .......... .......... .......... 38% 23.6M 9s
101900K .......... .......... .......... .......... .......... 38% 66.6M 9s
101950K .......... .......... .......... .......... .......... 38% 18.2M 9s
102000K .......... .......... .......... .......... .......... 38% 87.1M 9s
102050K .......... .......... .......... .......... .......... 38% 23.8M 9s
102100K .......... .......... .......... .......... .......... 38% 22.4M 9s
102150K .......... .......... .......... .......... .......... 38%  115M 9s
102200K .......... .......... .......... .......... .......... 38% 18.5M 9s
102250K .......... .......... .......... .......... .......... 38% 45.3M 9s
102300K .......... .......... .......... .......... .......... 38% 33.8M 9s
102350K .......... .......... .......... .......... .......... 38% 19.8M 9s
102400K .......... .......... .......... .......... .......... 38% 46.8M 9s
102450K .......... .......... .......... .......... .......... 38% 18.3M 9s
102500K .......... .......... .......... .......... .......... 38% 46.4M 9s
102550K .......... .......... .......... .......... .......... 38% 26.4M 9s
102600K .......... .......... .......... .......... .......... 38% 26.5M 9s
102650K .......... .......... .......... .......... .......... 38% 96.6M 9s
102700K .......... .......... .......... .......... .......... 38% 18.7M 8s
102750K .......... .......... .......... .......... .......... 38% 34.2M 8s
102800K .......... .......... .......... .......... .......... 38% 31.2M 8s
102850K .......... .......... .......... .......... .......... 38% 43.7M 8s
102900K .......... .......... .......... .......... .......... 38% 34.7M 8s
102950K .......... .......... .......... .......... .......... 38% 17.8M 8s
103000K .......... .......... .......... .......... .......... 38% 29.2M 8s
103050K .......... .......... .......... .......... .......... 38% 44.3M 8s
103100K .......... .......... .......... .......... .......... 38% 38.8M 8s
103150K .......... .......... .......... .......... .......... 38% 26.8M 8s
103200K .......... .......... .......... .......... .......... 38% 40.0M 8s
103250K .......... .......... .......... .......... .......... 38% 17.4M 8s
103300K .......... .......... .......... .......... .......... 38% 85.7M 8s
103350K .......... .......... .......... .......... .......... 38% 29.8M 8s
103400K .......... .......... .......... .......... .......... 38% 23.8M 8s
103450K .......... .......... .......... .......... .......... 38% 39.4M 8s
103500K .......... .......... .......... .......... .......... 38% 19.8M 8s
103550K .......... .......... .......... .......... .......... 38% 48.9M 8s
103600K .......... .......... .......... .......... .......... 38% 23.0M 8s
103650K .......... .......... .......... .......... .......... 39% 25.9M 8s
103700K .......... .......... .......... .......... .......... 39% 21.5M 8s
103750K .......... .......... .......... .......... .......... 39% 53.3M 8s
103800K .......... .......... .......... .......... .......... 39% 32.5M 8s
103850K .......... .......... .......... .......... .......... 39% 20.9M 8s
103900K .......... .......... .......... .......... .......... 39% 42.5M 8s
103950K .......... .......... .......... .......... .......... 39% 18.6M 8s
104000K .......... .......... .......... .......... .......... 39% 25.3M 8s
104050K .......... .......... .......... .......... .......... 39% 37.7M 8s
104100K .......... .......... .......... .......... .......... 39% 19.9M 8s
104150K .......... .......... .......... .......... .......... 39% 33.4M 8s
104200K .......... .......... .......... .......... .......... 39% 24.3M 8s
104250K .......... .......... .......... .......... .......... 39% 20.9M 8s
104300K .......... .......... .......... .......... .......... 39% 33.9M 8s
104350K .......... .......... .......... .......... .......... 39% 28.5M 8s
104400K .......... .......... .......... .......... .......... 39% 24.6M 8s
104450K .......... .......... .......... .......... .......... 39% 27.8M 8s
104500K .......... .......... .......... .......... .......... 39% 34.6M 8s
104550K .......... .......... .......... .......... .......... 39% 21.8M 8s
104600K .......... .......... .......... .......... .......... 39% 37.0M 8s
104650K .......... .......... .......... .......... .......... 39% 19.5M 8s
104700K .......... .......... .......... .......... .......... 39% 28.4M 8s
104750K .......... .......... .......... .......... .......... 39% 62.0M 8s
104800K .......... .......... .......... .......... .......... 39% 20.2M 8s
104850K .......... .......... .......... .......... .......... 39% 24.8M 8s
104900K .......... .......... .......... .......... .......... 39% 26.4M 8s
104950K .......... .......... .......... .......... .......... 39% 24.0M 8s
105000K .......... .......... .......... .......... .......... 39% 46.4M 8s
105050K .......... .......... .......... .......... .......... 39% 25.1M 8s
105100K .......... .......... .......... .......... .......... 39% 25.9M 8s
105150K .......... .......... .......... .......... .......... 39% 17.3M 8s
105200K .......... .......... .......... .......... .......... 39% 46.4M 8s
105250K .......... .......... .......... .......... .......... 39% 38.3M 8s
105300K .......... .......... .......... .......... .......... 39% 22.8M 8s
105350K .......... .......... .......... .......... .......... 39% 33.5M 8s
105400K .......... .......... .......... .......... .......... 39% 19.3M 8s
105450K .......... .......... .......... .......... .......... 39% 56.2M 8s
105500K .......... .......... .......... .......... .......... 39% 25.3M 8s
105550K .......... .......... .......... .......... .......... 39% 25.6M 8s
105600K .......... .......... .......... .......... .......... 39% 20.0M 8s
105650K .......... .......... .......... .......... .......... 39% 72.3M 8s
105700K .......... .......... .......... .......... .......... 39% 23.5M 8s
105750K .......... .......... .......... .......... .......... 39% 22.6M 8s
105800K .......... .......... .......... .......... .......... 39% 38.2M 8s
105850K .......... .......... .......... .......... .......... 39% 22.1M 8s
105900K .......... .......... .......... .......... .......... 39% 33.6M 8s
105950K .......... .......... .......... .......... .......... 39% 49.4M 8s
106000K .......... .......... .......... .......... .......... 39% 19.4M 8s
106050K .......... .......... .......... .......... .......... 39% 23.5M 8s
106100K .......... .......... .......... .......... .......... 39% 28.2M 8s
106150K .......... .......... .......... .......... .......... 39% 98.3M 8s
106200K .......... .......... .......... .......... .......... 39% 17.2M 8s
106250K .......... .......... .......... .......... .......... 39% 24.5M 8s
106300K .......... .......... .......... .......... .......... 40% 45.6M 8s
106350K .......... .......... .......... .......... .......... 40% 24.6M 8s
106400K .......... .......... .......... .......... .......... 40% 25.5M 8s
106450K .......... .......... .......... .......... .......... 40% 32.6M 8s
106500K .......... .......... .......... .......... .......... 40% 31.7M 8s
106550K .......... .......... .......... .......... .......... 40% 26.7M 8s
106600K .......... .......... .......... .......... .......... 40% 26.5M 8s
106650K .......... .......... .......... .......... .......... 40% 33.3M 8s
106700K .......... .......... .......... .......... .......... 40% 19.3M 8s
106750K .......... .......... .......... .......... .......... 40% 37.5M 8s
106800K .......... .......... .......... .......... .......... 40% 37.7M 8s
106850K .......... .......... .......... .......... .......... 40% 19.7M 8s
106900K .......... .......... .......... .......... .......... 40% 38.0M 8s
106950K .......... .......... .......... .......... .......... 40% 23.1M 8s
107000K .......... .......... .......... .......... .......... 40% 27.5M 8s
107050K .......... .......... .......... .......... .......... 40% 35.4M 8s
107100K .......... .......... .......... .......... .......... 40% 35.3M 8s
107150K .......... .......... .......... .......... .......... 40% 22.4M 8s
107200K .......... .......... .......... .......... .......... 40% 57.1M 8s
107250K .......... .......... .......... .......... .......... 40% 17.8M 8s
107300K .......... .......... .......... .......... .......... 40% 39.4M 8s
107350K .......... .......... .......... .......... .......... 40% 39.4M 8s
107400K .......... .......... .......... .......... .......... 40% 19.7M 8s
107450K .......... .......... .......... .......... .......... 40% 84.1M 8s
107500K .......... .......... .......... .......... .......... 40% 18.1M 8s
107550K .......... .......... .......... .......... .......... 40%  150M 8s
107600K .......... .......... .......... .......... .......... 40% 19.5M 8s
107650K .......... .......... .......... .......... .......... 40% 46.3M 8s
107700K .......... .......... .......... .......... .......... 40% 34.4M 8s
107750K .......... .......... .......... .......... .......... 40% 16.1M 8s
107800K .......... .......... .......... .......... .......... 40% 54.3M 8s
107850K .......... .......... .......... .......... .......... 40% 47.2M 8s
107900K .......... .......... .......... .......... .......... 40% 15.8M 8s
107950K .......... .......... .......... .......... .......... 40% 46.8M 8s
108000K .......... .......... .......... .......... .......... 40% 44.8M 8s
108050K .......... .......... .......... .......... .......... 40% 21.7M 8s
108100K .......... .......... .......... .......... .......... 40% 24.0M 8s
108150K .......... .......... .......... .......... .......... 40% 40.1M 8s
108200K .......... .......... .......... .......... .......... 40% 32.9M 8s
108250K .......... .......... .......... .......... .......... 40% 20.7M 8s
108300K .......... .......... .......... .......... .......... 40% 48.2M 8s
108350K .......... .......... .......... .......... .......... 40% 32.5M 8s
108400K .......... .......... .......... .......... .......... 40% 17.4M 8s
108450K .......... .......... .......... .......... .......... 40% 64.5M 8s
108500K .......... .......... .......... .......... .......... 40% 77.1M 8s
108550K .......... .......... .......... .......... .......... 40% 16.4M 8s
108600K .......... .......... .......... .......... .......... 40% 32.0M 8s
108650K .......... .......... .......... .......... .......... 40% 57.5M 8s
108700K .......... .......... .......... .......... .......... 40% 18.5M 8s
108750K .......... .......... .......... .......... .......... 40% 29.1M 8s
108800K .......... .......... .......... .......... .......... 40% 59.2M 8s
108850K .......... .......... .......... .......... .......... 40% 19.9M 8s
108900K .......... .......... .......... .......... .......... 40% 20.2M 8s
108950K .......... .......... .......... .......... .......... 41% 62.3M 8s
109000K .......... .......... .......... .......... .......... 41% 52.4M 8s
109050K .......... .......... .......... .......... .......... 41% 22.8M 8s
109100K .......... .......... .......... .......... .......... 41% 19.3M 8s
109150K .......... .......... .......... .......... .......... 41% 58.7M 8s
109200K .......... .......... .......... .......... .......... 41% 22.9M 8s
109250K .......... .......... .......... .......... .......... 41% 29.8M 8s
109300K .......... .......... .......... .......... .......... 41% 33.7M 8s
109350K .......... .......... .......... .......... .......... 41% 34.9M 8s
109400K .......... .......... .......... .......... .......... 41% 17.4M 8s
109450K .......... .......... .......... .......... .......... 41% 72.5M 8s
109500K .......... .......... .......... .......... .......... 41% 26.7M 8s
109550K .......... .......... .......... .......... .......... 41% 18.9M 8s
109600K .......... .......... .......... .......... .......... 41% 42.4M 8s
109650K .......... .......... .......... .......... .......... 41% 40.9M 8s
109700K .......... .......... .......... .......... .......... 41% 32.3M 8s
109750K .......... .......... .......... .......... .......... 41% 18.5M 8s
109800K .......... .......... .......... .......... .......... 41% 31.6M 8s
109850K .......... .......... .......... .......... .......... 41% 42.6M 8s
109900K .......... .......... .......... .......... .......... 41% 20.4M 8s
109950K .......... .......... .......... .......... .......... 41% 36.8M 8s
110000K .......... .......... .......... .......... .......... 41% 36.2M 8s
110050K .......... .......... .......... .......... .......... 41% 17.5M 8s
110100K .......... .......... .......... .......... .......... 41% 39.8M 8s
110150K .......... .......... .......... .......... .......... 41%  123M 8s
110200K .......... .......... .......... .......... .......... 41% 21.4M 8s
110250K .......... .......... .......... .......... .......... 41% 20.5M 8s
110300K .......... .......... .......... .......... .......... 41% 59.7M 8s
110350K .......... .......... .......... .......... .......... 41% 29.0M 8s
110400K .......... .......... .......... .......... .......... 41% 25.2M 8s
110450K .......... .......... .......... .......... .......... 41% 43.1M 8s
110500K .......... .......... .......... .......... .......... 41% 46.6M 8s
110550K .......... .......... .......... .......... .......... 41% 21.8M 8s
110600K .......... .......... .......... .......... .......... 41% 32.4M 8s
110650K .......... .......... .......... .......... .......... 41% 37.7M 8s
110700K .......... .......... .......... .......... .......... 41% 29.0M 8s
110750K .......... .......... .......... .......... .......... 41% 29.5M 8s
110800K .......... .......... .......... .......... .......... 41% 39.9M 8s
110850K .......... .......... .......... .......... .......... 41% 29.3M 8s
110900K .......... .......... .......... .......... .......... 41% 29.0M 8s
110950K .......... .......... .......... .......... .......... 41% 62.1M 8s
111000K .......... .......... .......... .......... .......... 41% 37.6M 8s
111050K .......... .......... .......... .......... .......... 41% 18.5M 8s
111100K .......... .......... .......... .......... .......... 41% 79.3M 8s
111150K .......... .......... .......... .......... .......... 41% 55.2M 8s
111200K .......... .......... .......... .......... .......... 41% 30.1M 8s
111250K .......... .......... .......... .......... .......... 41% 25.6M 8s
111300K .......... .......... .......... .......... .......... 41% 45.8M 8s
111350K .......... .......... .......... .......... .......... 41% 30.5M 8s
111400K .......... .......... .......... .......... .......... 41% 27.8M 8s
111450K .......... .......... .......... .......... .......... 41% 70.6M 8s
111500K .......... .......... .......... .......... .......... 41% 32.1M 8s
111550K .......... .......... .......... .......... .......... 41% 27.9M 8s
111600K .......... .......... .......... .......... .......... 42% 34.2M 8s
111650K .......... .......... .......... .......... .......... 42%  108M 8s
111700K .......... .......... .......... .......... .......... 42% 24.5M 8s
111750K .......... .......... .......... .......... .......... 42% 21.3M 8s
111800K .......... .......... .......... .......... .......... 42%  141M 8s
111850K .......... .......... .......... .......... .......... 42% 30.5M 8s
111900K .......... .......... .......... .......... .......... 42% 27.4M 8s
111950K .......... .......... .......... .......... .......... 42% 36.9M 8s
112000K .......... .......... .......... .......... .......... 42% 31.6M 8s
112050K .......... .......... .......... .......... .......... 42% 30.3M 8s
112100K .......... .......... .......... .......... .......... 42% 35.8M 8s
112150K .......... .......... .......... .......... .......... 42% 28.6M 8s
112200K .......... .......... .......... .......... .......... 42% 31.6M 8s
112250K .......... .......... .......... .......... .......... 42% 33.8M 8s
112300K .......... .......... .......... .......... .......... 42% 32.8M 8s
112350K .......... .......... .......... .......... .......... 42% 64.8M 8s
112400K .......... .......... .......... .......... .......... 42% 24.8M 8s
112450K .......... .......... .......... .......... .......... 42% 23.0M 8s
112500K .......... .......... .......... .......... .......... 42% 43.7M 8s
112550K .......... .......... .......... .......... .......... 42% 66.9M 8s
112600K .......... .......... .......... .......... .......... 42% 28.3M 8s
112650K .......... .......... .......... .......... .......... 42% 30.1M 8s
112700K .......... .......... .......... .......... .......... 42% 24.8M 8s
112750K .......... .......... .......... .......... .......... 42% 46.7M 8s
112800K .......... .......... .......... .......... .......... 42% 38.0M 8s
112850K .......... .......... .......... .......... .......... 42% 31.0M 8s
112900K .......... .......... .......... .......... .......... 42% 38.1M 8s
112950K .......... .......... .......... .......... .......... 42% 20.7M 8s
113000K .......... .......... .......... .......... .......... 42% 50.9M 8s
113050K .......... .......... .......... .......... .......... 42% 37.0M 8s
113100K .......... .......... .......... .......... .......... 42% 36.0M 8s
113150K .......... .......... .......... .......... .......... 42% 22.9M 8s
113200K .......... .......... .......... .......... .......... 42% 43.7M 8s
113250K .......... .......... .......... .......... .......... 42% 47.0M 8s
113300K .......... .......... .......... .......... .......... 42% 31.3M 8s
113350K .......... .......... .......... .......... .......... 42% 26.2M 8s
113400K .......... .......... .......... .......... .......... 42% 50.9M 8s
113450K .......... .......... .......... .......... .......... 42% 26.7M 8s
113500K .......... .......... .......... .......... .......... 42% 28.0M 8s
113550K .......... .......... .......... .......... .......... 42% 57.7M 8s
113600K .......... .......... .......... .......... .......... 42% 48.4M 8s
113650K .......... .......... .......... .......... .......... 42% 22.0M 8s
113700K .......... .......... .......... .......... .......... 42% 35.1M 8s
113750K .......... .......... .......... .......... .......... 42% 75.1M 8s
113800K .......... .......... .......... .......... .......... 42% 45.8M 8s
113850K .......... .......... .......... .......... .......... 42% 16.2M 8s
113900K .......... .......... .......... .......... .......... 42% 54.1M 8s
113950K .......... .......... .......... .......... .......... 42% 70.1M 8s
114000K .......... .......... .......... .......... .......... 42% 44.7M 8s
114050K .......... .......... .......... .......... .......... 42% 18.4M 8s
114100K .......... .......... .......... .......... .......... 42% 51.1M 8s
114150K .......... .......... .......... .......... .......... 42% 83.1M 8s
114200K .......... .......... .......... .......... .......... 42% 34.2M 8s
114250K .......... .......... .......... .......... .......... 43% 16.9M 8s
114300K .......... .......... .......... .......... .......... 43% 91.5M 8s
114350K .......... .......... .......... .......... .......... 43% 34.6M 8s
114400K .......... .......... .......... .......... .......... 43% 58.4M 8s
114450K .......... .......... .......... .......... .......... 43% 18.0M 8s
114500K .......... .......... .......... .......... .......... 43% 24.8M 8s
114550K .......... .......... .......... .......... .......... 43% 39.3M 8s
114600K .......... .......... .......... .......... .......... 43% 39.0M 8s
114650K .......... .......... .......... .......... .......... 43% 63.8M 8s
114700K .......... .......... .......... .......... .......... 43% 40.0M 8s
114750K .......... .......... .......... .......... .......... 43% 62.4M 8s
114800K .......... .......... .......... .......... .......... 43% 16.0M 8s
114850K .......... .......... .......... .......... .......... 43% 30.9M 8s
114900K .......... .......... .......... .......... .......... 43% 38.2M 8s
114950K .......... .......... .......... .......... .......... 43% 31.7M 8s
115000K .......... .......... .......... .......... .......... 43% 39.4M 8s
115050K .......... .......... .......... .......... .......... 43% 42.1M 8s
115100K .......... .......... .......... .......... .......... 43% 35.3M 8s
115150K .......... .......... .......... .......... .......... 43% 34.8M 8s
115200K .......... .......... .......... .......... .......... 43% 27.9M 8s
115250K .......... .......... .......... .......... .......... 43% 89.9M 8s
115300K .......... .......... .......... .......... .......... 43% 61.5M 8s
115350K .......... .......... .......... .......... .......... 43% 51.5M 8s
115400K .......... .......... .......... .......... .......... 43% 18.8M 8s
115450K .......... .......... .......... .......... .......... 43% 39.1M 8s
115500K .......... .......... .......... .......... .......... 43% 41.2M 7s
115550K .......... .......... .......... .......... .......... 43% 21.5M 7s
115600K .......... .......... .......... .......... .......... 43% 50.9M 7s
115650K .......... .......... .......... .......... .......... 43% 39.7M 7s
115700K .......... .......... .......... .......... .......... 43% 43.0M 7s
115750K .......... .......... .......... .......... .......... 43% 21.1M 7s
115800K .......... .......... .......... .......... .......... 43% 56.2M 7s
115850K .......... .......... .......... .......... .......... 43% 29.6M 7s
115900K .......... .......... .......... .......... .......... 43% 74.4M 7s
115950K .......... .......... .......... .......... .......... 43% 21.5M 7s
116000K .......... .......... .......... .......... .......... 43% 30.2M 7s
116050K .......... .......... .......... .......... .......... 43% 43.6M 7s
116100K .......... .......... .......... .......... .......... 43% 45.4M 7s
116150K .......... .......... .......... .......... .......... 43% 28.6M 7s
116200K .......... .......... .......... .......... .......... 43% 31.5M 7s
116250K .......... .......... .......... .......... .......... 43% 45.9M 7s
116300K .......... .......... .......... .......... .......... 43% 70.5M 7s
116350K .......... .......... .......... .......... .......... 43% 5.97M 7s
116400K .......... .......... .......... .......... .......... 43% 70.5M 7s
116450K .......... .......... .......... .......... .......... 43% 91.8M 7s
116500K .......... .......... .......... .......... .......... 43% 51.3M 7s
116550K .......... .......... .......... .......... .......... 43% 78.2M 7s
116600K .......... .......... .......... .......... .......... 43% 91.1M 7s
116650K .......... .......... .......... .......... .......... 43% 83.2M 7s
116700K .......... .......... .......... .......... .......... 43% 55.4M 7s
116750K .......... .......... .......... .......... .......... 43% 40.9M 7s
116800K .......... .......... .......... .......... .......... 43% 33.6M 7s
116850K .......... .......... .......... .......... .......... 43% 46.6M 7s
116900K .......... .......... .......... .......... .......... 43% 24.8M 7s
116950K .......... .......... .......... .......... .......... 44% 39.0M 7s
117000K .......... .......... .......... .......... .......... 44% 43.8M 7s
117050K .......... .......... .......... .......... .......... 44% 22.5M 7s
117100K .......... .......... .......... .......... .......... 44% 45.6M 7s
117150K .......... .......... .......... .......... .......... 44% 22.2M 7s
117200K .......... .......... .......... .......... .......... 44% 36.0M 7s
117250K .......... .......... .......... .......... .......... 44% 59.3M 7s
117300K .......... .......... .......... .......... .......... 44% 45.6M 7s
117350K .......... .......... .......... .......... .......... 44% 57.8M 7s
117400K .......... .......... .......... .......... .......... 44% 67.5M 7s
117450K .......... .......... .......... .......... .......... 44% 55.2M 7s
117500K .......... .......... .......... .......... .......... 44% 58.8M 7s
117550K .......... .......... .......... .......... .......... 44% 32.8M 7s
117600K .......... .......... .......... .......... .......... 44% 33.6M 7s
117650K .......... .......... .......... .......... .......... 44% 21.8M 7s
117700K .......... .......... .......... .......... .......... 44% 41.3M 7s
117750K .......... .......... .......... .......... .......... 44%  142M 7s
117800K .......... .......... .......... .......... .......... 44% 21.2M 7s
117850K .......... .......... .......... .......... .......... 44% 42.6M 7s
117900K .......... .......... .......... .......... .......... 44% 28.8M 7s
117950K .......... .......... .......... .......... .......... 44% 63.7M 7s
118000K .......... .......... .......... .......... .......... 44% 43.0M 7s
118050K .......... .......... .......... .......... .......... 44% 14.6M 7s
118100K .......... .......... .......... .......... .......... 44% 86.4M 7s
118150K .......... .......... .......... .......... .......... 44% 29.2M 7s
118200K .......... .......... .......... .......... .......... 44% 23.0M 7s
118250K .......... .......... .......... .......... .......... 44%  101M 7s
118300K .......... .......... .......... .......... .......... 44% 44.1M 7s
118350K .......... .......... .......... .......... .......... 44% 18.7M 7s
118400K .......... .......... .......... .......... .......... 44%  109M 7s
118450K .......... .......... .......... .......... .......... 44% 24.4M 7s
118500K .......... .......... .......... .......... .......... 44% 37.4M 7s
118550K .......... .......... .......... .......... .......... 44% 37.3M 7s
118600K .......... .......... .......... .......... .......... 44% 30.2M 7s
118650K .......... .......... .......... .......... .......... 44%  108M 7s
118700K .......... .......... .......... .......... .......... 44% 28.7M 7s
118750K .......... .......... .......... .......... .......... 44% 24.0M 7s
118800K .......... .......... .......... .......... .......... 44% 43.1M 7s
118850K .......... .......... .......... .......... .......... 44% 22.7M 7s
118900K .......... .......... .......... .......... .......... 44% 40.3M 7s
118950K .......... .......... .......... .......... .......... 44% 27.7M 7s
119000K .......... .......... .......... .......... .......... 44% 35.9M 7s
119050K .......... .......... .......... .......... .......... 44% 30.8M 7s
119100K .......... .......... .......... .......... .......... 44% 42.3M 7s
119150K .......... .......... .......... .......... .......... 44% 33.7M 7s
119200K .......... .......... .......... .......... .......... 44% 26.7M 7s
119250K .......... .......... .......... .......... .......... 44% 44.8M 7s
119300K .......... .......... .......... .......... .......... 44% 15.9M 7s
119350K .......... .......... .......... .......... .......... 44% 32.7M 7s
119400K .......... .......... .......... .......... .......... 44% 46.5M 7s
119450K .......... .......... .......... .......... .......... 44% 33.3M 7s
119500K .......... .......... .......... .......... .......... 44% 42.1M 7s
119550K .......... .......... .......... .......... .......... 44% 24.4M 7s
119600K .......... .......... .......... .......... .......... 45% 34.2M 7s
119650K .......... .......... .......... .......... .......... 45% 66.9M 7s
119700K .......... .......... .......... .......... .......... 45% 24.7M 7s
119750K .......... .......... .......... .......... .......... 45% 20.0M 7s
119800K .......... .......... .......... .......... .......... 45% 27.4M 7s
119850K .......... .......... .......... .......... .......... 45% 41.7M 7s
119900K .......... .......... .......... .......... .......... 45% 20.2M 7s
119950K .......... .......... .......... .......... .......... 45% 92.2M 7s
120000K .......... .......... .......... .......... .......... 45% 33.8M 7s
120050K .......... .......... .......... .......... .......... 45% 71.1M 7s
120100K .......... .......... .......... .......... .......... 45% 24.8M 7s
120150K .......... .......... .......... .......... .......... 45% 44.8M 7s
120200K .......... .......... .......... .......... .......... 45% 37.8M 7s
120250K .......... .......... .......... .......... .......... 45% 16.2M 7s
120300K .......... .......... .......... .......... .......... 45%  112M 7s
120350K .......... .......... .......... .......... .......... 45% 26.6M 7s
120400K .......... .......... .......... .......... .......... 45% 25.4M 7s
120450K .......... .......... .......... .......... .......... 45% 36.6M 7s
120500K .......... .......... .......... .......... .......... 45% 32.5M 7s
120550K .......... .......... .......... .......... .......... 45% 39.4M 7s
120600K .......... .......... .......... .......... .......... 45% 25.8M 7s
120650K .......... .......... .......... .......... .......... 45% 34.7M 7s
120700K .......... .......... .......... .......... .......... 45% 26.7M 7s
120750K .......... .......... .......... .......... .......... 45% 27.7M 7s
120800K .......... .......... .......... .......... .......... 45% 33.2M 7s
120850K .......... .......... .......... .......... .......... 45% 25.0M 7s
120900K .......... .......... .......... .......... .......... 45% 26.1M 7s
120950K .......... .......... .......... .......... .......... 45% 43.0M 7s
121000K .......... .......... .......... .......... .......... 45% 65.5M 7s
121050K .......... .......... .......... .......... .......... 45% 21.0M 7s
121100K .......... .......... .......... .......... .......... 45% 21.5M 7s
121150K .......... .......... .......... .......... .......... 45% 20.8M 7s
121200K .......... .......... .......... .......... .......... 45% 44.8M 7s
121250K .......... .......... .......... .......... .......... 45%  131M 7s
121300K .......... .......... .......... .......... .......... 45% 29.7M 7s
121350K .......... .......... .......... .......... .......... 45% 70.9M 7s
121400K .......... .......... .......... .......... .......... 45% 63.8M 7s
121450K .......... .......... .......... .......... .......... 45% 36.6M 7s
121500K .......... .......... .......... .......... .......... 45% 49.7M 7s
121550K .......... .......... .......... .......... .......... 45% 23.4M 7s
121600K .......... .......... .......... .......... .......... 45% 48.4M 7s
121650K .......... .......... .......... .......... .......... 45% 33.3M 7s
121700K .......... .......... .......... .......... .......... 45%  104M 7s
121750K .......... .......... .......... .......... .......... 45% 46.3M 7s
121800K .......... .......... .......... .......... .......... 45%  138M 7s
121850K .......... .......... .......... .......... .......... 45% 44.4M 7s
121900K .......... .......... .......... .......... .......... 45% 81.8M 7s
121950K .......... .......... .......... .......... .......... 45% 42.4M 7s
122000K .......... .......... .......... .......... .......... 45% 16.1M 7s
122050K .......... .......... .......... .......... .......... 45%  115M 7s
122100K .......... .......... .......... .......... .......... 45% 28.9M 7s
122150K .......... .......... .......... .......... .......... 45% 24.7M 7s
122200K .......... .......... .......... .......... .......... 45% 32.2M 7s
122250K .......... .......... .......... .......... .......... 46% 21.6M 7s
122300K .......... .......... .......... .......... .......... 46% 33.6M 7s
122350K .......... .......... .......... .......... .......... 46% 24.9M 7s
122400K .......... .......... .......... .......... .......... 46% 35.6M 7s
122450K .......... .......... .......... .......... .......... 46% 31.3M 7s
122500K .......... .......... .......... .......... .......... 46% 37.7M 7s
122550K .......... .......... .......... .......... .......... 46% 30.9M 7s
122600K .......... .......... .......... .......... .......... 46% 23.8M 7s
122650K .......... .......... .......... .......... .......... 46% 22.4M 7s
122700K .......... .......... .......... .......... .......... 46% 21.9M 7s
122750K .......... .......... .......... .......... .......... 46% 50.3M 7s
122800K .......... .......... .......... .......... .......... 46% 18.6M 7s
122850K .......... .......... .......... .......... .......... 46% 33.1M 7s
122900K .......... .......... .......... .......... .......... 46% 15.1M 7s
122950K .......... .......... .......... .......... .......... 46% 18.7M 7s
123000K .......... .......... .......... .......... .......... 46% 36.4M 7s
123050K .......... .......... .......... .......... .......... 46% 66.4M 7s
123100K .......... .......... .......... .......... .......... 46% 33.1M 7s
123150K .......... .......... .......... .......... .......... 46% 20.9M 7s
123200K .......... .......... .......... .......... .......... 46% 31.0M 7s
123250K .......... .......... .......... .......... .......... 46% 33.7M 7s
123300K .......... .......... .......... .......... .......... 46% 18.4M 7s
123350K .......... .......... .......... .......... .......... 46% 38.7M 7s
123400K .......... .......... .......... .......... .......... 46% 32.9M 7s
123450K .......... .......... .......... .......... .......... 46% 63.5M 7s
123500K .......... .......... .......... .......... .......... 46% 18.0M 7s
123550K .......... .......... .......... .......... .......... 46% 26.8M 7s
123600K .......... .......... .......... .......... .......... 46% 21.6M 7s
123650K .......... .......... .......... .......... .......... 46%  125M 7s
123700K .......... .......... .......... .......... .......... 46% 16.6M 7s
123750K .......... .......... .......... .......... .......... 46% 32.0M 7s
123800K .......... .......... .......... .......... .......... 46% 22.8M 7s
123850K .......... .......... .......... .......... .......... 46% 31.0M 7s
123900K .......... .......... .......... .......... .......... 46% 62.9M 7s
123950K .......... .......... .......... .......... .......... 46% 21.8M 7s
124000K .......... .......... .......... .......... .......... 46% 25.2M 7s
124050K .......... .......... .......... .......... .......... 46% 28.3M 7s
124100K .......... .......... .......... .......... .......... 46% 21.8M 7s
124150K .......... .......... .......... .......... .......... 46% 37.7M 7s
124200K .......... .......... .......... .......... .......... 46% 20.0M 7s
124250K .......... .......... .......... .......... .......... 46% 44.0M 7s
124300K .......... .......... .......... .......... .......... 46% 24.5M 7s
124350K .......... .......... .......... .......... .......... 46% 16.3M 7s
124400K .......... .......... .......... .......... .......... 46% 43.3M 7s
124450K .......... .......... .......... .......... .......... 46% 31.0M 7s
124500K .......... .......... .......... .......... .......... 46% 21.7M 7s
124550K .......... .......... .......... .......... .......... 46% 23.9M 7s
124600K .......... .......... .......... .......... .......... 46% 47.3M 7s
124650K .......... .......... .......... .......... .......... 46% 34.7M 7s
124700K .......... .......... .......... .......... .......... 46% 20.7M 7s
124750K .......... .......... .......... .......... .......... 46% 33.8M 7s
124800K .......... .......... .......... .......... .......... 46% 30.0M 7s
124850K .......... .......... .......... .......... .......... 46% 32.5M 7s
124900K .......... .......... .......... .......... .......... 47% 29.4M 7s
124950K .......... .......... .......... .......... .......... 47% 26.2M 7s
125000K .......... .......... .......... .......... .......... 47% 23.5M 7s
125050K .......... .......... .......... .......... .......... 47% 18.9M 7s
125100K .......... .......... .......... .......... .......... 47% 48.4M 7s
125150K .......... .......... .......... .......... .......... 47% 22.5M 7s
125200K .......... .......... .......... .......... .......... 47% 21.2M 7s
125250K .......... .......... .......... .......... .......... 47% 25.8M 7s
125300K .......... .......... .......... .......... .......... 47%  124M 7s
125350K .......... .......... .......... .......... .......... 47% 24.0M 7s
125400K .......... .......... .......... .......... .......... 47% 26.3M 7s
125450K .......... .......... .......... .......... .......... 47% 21.4M 7s
125500K .......... .......... .......... .......... .......... 47% 23.5M 7s
125550K .......... .......... .......... .......... .......... 47% 54.1M 7s
125600K .......... .......... .......... .......... .......... 47% 34.7M 7s
125650K .......... .......... .......... .......... .......... 47% 27.1M 7s
125700K .......... .......... .......... .......... .......... 47% 24.9M 7s
125750K .......... .......... .......... .......... .......... 47% 25.6M 7s
125800K .......... .......... .......... .......... .......... 47% 61.1M 7s
125850K .......... .......... .......... .......... .......... 47% 16.0M 7s
125900K .......... .......... .......... .......... .......... 47% 28.8M 7s
125950K .......... .......... .......... .......... .......... 47% 20.7M 7s
126000K .......... .......... .......... .......... .......... 47% 34.1M 7s
126050K .......... .......... .......... .......... .......... 47% 85.8M 7s
126100K .......... .......... .......... .......... .......... 47% 23.8M 7s
126150K .......... .......... .......... .......... .......... 47% 26.0M 7s
126200K .......... .......... .......... .......... .......... 47% 22.3M 7s
126250K .......... .......... .......... .......... .......... 47% 79.9M 7s
126300K .......... .......... .......... .......... .......... 47% 17.5M 7s
126350K .......... .......... .......... .......... .......... 47% 34.6M 7s
126400K .......... .......... .......... .......... .......... 47% 22.3M 7s
126450K .......... .......... .......... .......... .......... 47% 36.7M 7s
126500K .......... .......... .......... .......... .......... 47% 48.2M 7s
126550K .......... .......... .......... .......... .......... 47% 25.9M 7s
126600K .......... .......... .......... .......... .......... 47% 21.9M 7s
126650K .......... .......... .......... .......... .......... 47% 24.4M 7s
126700K .......... .......... .......... .......... .......... 47% 21.9M 7s
126750K .......... .......... .......... .......... .......... 47% 45.5M 7s
126800K .......... .......... .......... .......... .......... 47% 23.9M 7s
126850K .......... .......... .......... .......... .......... 47% 23.1M 7s
126900K .......... .......... .......... .......... .......... 47% 21.3M 7s
126950K .......... .......... .......... .......... .......... 47% 29.3M 7s
127000K .......... .......... .......... .......... .......... 47% 57.0M 7s
127050K .......... .......... .......... .......... .......... 47% 29.9M 7s
127100K .......... .......... .......... .......... .......... 47% 23.4M 7s
127150K .......... .......... .......... .......... .......... 47% 23.0M 7s
127200K .......... .......... .......... .......... .......... 47% 56.8M 7s
127250K .......... .......... .......... .......... .......... 47% 19.6M 7s
127300K .......... .......... .......... .......... .......... 47% 35.9M 7s
127350K .......... .......... .......... .......... .......... 47% 19.7M 7s
127400K .......... .......... .......... .......... .......... 47% 30.4M 7s
127450K .......... .......... .......... .......... .......... 47% 61.0M 7s
127500K .......... .......... .......... .......... .......... 47% 19.5M 7s
127550K .......... .......... .......... .......... .......... 48% 23.8M 7s
127600K .......... .......... .......... .......... .......... 48% 30.3M 7s
127650K .......... .......... .......... .......... .......... 48% 59.2M 7s
127700K .......... .......... .......... .......... .......... 48% 21.7M 7s
127750K .......... .......... .......... .......... .......... 48% 26.5M 7s
127800K .......... .......... .......... .......... .......... 48% 24.4M 7s
127850K .......... .......... .......... .......... .......... 48% 24.0M 7s
127900K .......... .......... .......... .......... .......... 48%  101M 7s
127950K .......... .......... .......... .......... .......... 48% 21.7M 7s
128000K .......... .......... .......... .......... .......... 48% 26.3M 7s
128050K .......... .......... .......... .......... .......... 48% 19.2M 7s
128100K .......... .......... .......... .......... .......... 48% 22.3M 7s
128150K .......... .......... .......... .......... .......... 48% 42.0M 7s
128200K .......... .......... .......... .......... .......... 48% 14.6M 7s
128250K .......... .......... .......... .......... .......... 48% 60.9M 7s
128300K .......... .......... .......... .......... .......... 48% 25.3M 7s
128350K .......... .......... .......... .......... .......... 48% 24.4M 7s
128400K .......... .......... .......... .......... .......... 48% 71.6M 7s
128450K .......... .......... .......... .......... .......... 48% 30.6M 7s
128500K .......... .......... .......... .......... .......... 48% 9.16M 7s
128550K .......... .......... .......... .......... .......... 48%  109M 7s
128600K .......... .......... .......... .......... .......... 48% 66.5M 7s
128650K .......... .......... .......... .......... .......... 48%  145M 7s
128700K .......... .......... .......... .......... .......... 48% 8.66M 7s
128750K .......... .......... .......... .......... .......... 48%  112M 7s
128800K .......... .......... .......... .......... .......... 48%  120M 7s
128850K .......... .......... .......... .......... .......... 48% 34.9M 7s
128900K .......... .......... .......... .......... .......... 48% 23.2M 7s
128950K .......... .......... .......... .......... .......... 48% 14.4M 7s
129000K .......... .......... .......... .......... .......... 48% 24.0M 7s
129050K .......... .......... .......... .......... .......... 48% 28.0M 7s
129100K .......... .......... .......... .......... .......... 48% 11.9M 7s
129150K .......... .......... .......... .......... .......... 48% 22.6M 7s
129200K .......... .......... .......... .......... .......... 48% 14.9M 7s
129250K .......... .......... .......... .......... .......... 48% 29.2M 7s
129300K .......... .......... .......... .......... .......... 48% 21.7M 7s
129350K .......... .......... .......... .......... .......... 48% 42.2M 7s
129400K .......... .......... .......... .......... .......... 48% 18.1M 7s
129450K .......... .......... .......... .......... .......... 48% 26.1M 7s
129500K .......... .......... .......... .......... .......... 48% 14.4M 7s
129550K .......... .......... .......... .......... .......... 48% 14.0M 7s
129600K .......... .......... .......... .......... .......... 48% 41.3M 7s
129650K .......... .......... .......... .......... .......... 48% 16.1M 7s
129700K .......... .......... .......... .......... .......... 48% 15.3M 7s
129750K .......... .......... .......... .......... .......... 48% 27.8M 7s
129800K .......... .......... .......... .......... .......... 48% 26.5M 7s
129850K .......... .......... .......... .......... .......... 48% 15.4M 7s
129900K .......... .......... .......... .......... .......... 48% 18.6M 7s
129950K .......... .......... .......... .......... .......... 48% 15.9M 7s
130000K .......... .......... .......... .......... .......... 48% 36.2M 7s
130050K .......... .......... .......... .......... .......... 48% 13.0M 7s
130100K .......... .......... .......... .......... .......... 48% 17.5M 7s
130150K .......... .......... .......... .......... .......... 48% 28.6M 7s
130200K .......... .......... .......... .......... .......... 49% 14.4M 7s
130250K .......... .......... .......... .......... .......... 49% 39.4M 7s
130300K .......... .......... .......... .......... .......... 49% 11.8M 7s
130350K .......... .......... .......... .......... .......... 49% 29.8M 7s
130400K .......... .......... .......... .......... .......... 49% 16.3M 7s
130450K .......... .......... .......... .......... .......... 49% 20.6M 7s
130500K .......... .......... .......... .......... .......... 49% 21.4M 7s
130550K .......... .......... .......... .......... .......... 49% 19.6M 7s
130600K .......... .......... .......... .......... .......... 49% 15.1M 6s
130650K .......... .......... .......... .......... .......... 49% 18.0M 6s
130700K .......... .......... .......... .......... .......... 49% 15.9M 6s
130750K .......... .......... .......... .......... .......... 49% 23.4M 6s
130800K .......... .......... .......... .......... .......... 49% 21.8M 6s
130850K .......... .......... .......... .......... .......... 49% 15.9M 6s
130900K .......... .......... .......... .......... .......... 49% 16.5M 6s
130950K .......... .......... .......... .......... .......... 49% 20.2M 6s
131000K .......... .......... .......... .......... .......... 49% 19.6M 6s
131050K .......... .......... .......... .......... .......... 49% 21.8M 6s
131100K .......... .......... .......... .......... .......... 49% 20.9M 6s
131150K .......... .......... .......... .......... .......... 49% 21.8M 6s
131200K .......... .......... .......... .......... .......... 49% 15.6M 6s
131250K .......... .......... .......... .......... .......... 49% 14.0M 6s
131300K .......... .......... .......... .......... .......... 49% 37.9M 6s
131350K .......... .......... .......... .......... .......... 49% 13.8M 6s
131400K .......... .......... .......... .......... .......... 49% 35.8M 6s
131450K .......... .......... .......... .......... .......... 49% 13.8M 6s
131500K .......... .......... .......... .......... .......... 49% 21.4M 6s
131550K .......... .......... .......... .......... .......... 49% 19.8M 6s
131600K .......... .......... .......... .......... .......... 49% 20.6M 6s
131650K .......... .......... .......... .......... .......... 49% 18.1M 6s
131700K .......... .......... .......... .......... .......... 49% 19.1M 6s
131750K .......... .......... .......... .......... .......... 49% 16.3M 6s
131800K .......... .......... .......... .......... .......... 49% 36.3M 6s
131850K .......... .......... .......... .......... .......... 49% 15.3M 6s
131900K .......... .......... .......... .......... .......... 49% 23.1M 6s
131950K .......... .......... .......... .......... .......... 49% 18.4M 6s
132000K .......... .......... .......... .......... .......... 49% 17.3M 6s
132050K .......... .......... .......... .......... .......... 49% 26.0M 6s
132100K .......... .......... .......... .......... .......... 49% 16.7M 6s
132150K .......... .......... .......... .......... .......... 49% 22.5M 6s
132200K .......... .......... .......... .......... .......... 49% 12.2M 6s
132250K .......... .......... .......... .......... .......... 49% 65.1M 6s
132300K .......... .......... .......... .......... .......... 49% 14.4M 6s
132350K .......... .......... .......... .......... .......... 49% 45.8M 6s
132400K .......... .......... .......... .......... .......... 49% 26.2M 6s
132450K .......... .......... .......... .......... .......... 49% 17.2M 6s
132500K .......... .......... .......... .......... .......... 49% 45.8M 6s
132550K .......... .......... .......... .......... .......... 49% 32.7M 6s
132600K .......... .......... .......... .......... .......... 49% 58.0M 6s
132650K .......... .......... .......... .......... .......... 49%  134M 6s
132700K .......... .......... .......... .......... .......... 49% 24.0M 6s
132750K .......... .......... .......... .......... .......... 49% 25.1M 6s
132800K .......... .......... .......... .......... .......... 49% 34.6M 6s
132850K .......... .......... .......... .......... .......... 49% 23.6M 6s
132900K .......... .......... .......... .......... .......... 50% 25.7M 6s
132950K .......... .......... .......... .......... .......... 50% 40.2M 6s
133000K .......... .......... .......... .......... .......... 50% 19.8M 6s
133050K .......... .......... .......... .......... .......... 50% 39.6M 6s
133100K .......... .......... .......... .......... .......... 50% 22.0M 6s
133150K .......... .......... .......... .......... .......... 50% 37.2M 6s
133200K .......... .......... .......... .......... .......... 50% 41.9M 6s
133250K .......... .......... .......... .......... .......... 50% 30.6M 6s
133300K .......... .......... .......... .......... .......... 50% 22.0M 6s
133350K .......... .......... .......... .......... .......... 50% 22.0M 6s
133400K .......... .......... .......... .......... .......... 50% 92.4M 6s
133450K .......... .......... .......... .......... .......... 50% 18.1M 6s
133500K .......... .......... .......... .......... .......... 50% 28.7M 6s
133550K .......... .......... .......... .......... .......... 50% 33.0M 6s
133600K .......... .......... .......... .......... .......... 50% 17.8M 6s
133650K .......... .......... .......... .......... .......... 50% 7.64M 6s
133700K .......... .......... .......... .......... .......... 50% 75.7M 6s
133750K .......... .......... .......... .......... .......... 50%  211M 6s
133800K .......... .......... .......... .......... .......... 50%  183M 6s
133850K .......... .......... .......... .......... .......... 50% 25.5M 6s
133900K .......... .......... .......... .......... .......... 50%  115M 6s
133950K .......... .......... .......... .......... .......... 50% 46.1M 6s
134000K .......... .......... .......... .......... .......... 50% 10.2M 6s
134050K .......... .......... .......... .......... .......... 50% 62.0M 6s
134100K .......... .......... .......... .......... .......... 50% 66.2M 6s
134150K .......... .......... .......... .......... .......... 50% 68.0M 6s
134200K .......... .......... .......... .......... .......... 50% 50.3M 6s
134250K .......... .......... .......... .......... .......... 50%  111M 6s
134300K .......... .......... .......... .......... .......... 50%  133M 6s
134350K .......... .......... .......... .......... .......... 50% 16.6M 6s
134400K .......... .......... .......... .......... .......... 50% 79.2M 6s
134450K .......... .......... .......... .......... .......... 50% 25.5M 6s
134500K .......... .......... .......... .......... .......... 50% 37.0M 6s
134550K .......... .......... .......... .......... .......... 50% 26.6M 6s
134600K .......... .......... .......... .......... .......... 50% 37.5M 6s
134650K .......... .......... .......... .......... .......... 50% 28.1M 6s
134700K .......... .......... .......... .......... .......... 50% 31.5M 6s
134750K .......... .......... .......... .......... .......... 50% 30.3M 6s
134800K .......... .......... .......... .......... .......... 50% 38.1M 6s
134850K .......... .......... .......... .......... .......... 50% 25.4M 6s
134900K .......... .......... .......... .......... .......... 50% 34.4M 6s
134950K .......... .......... .......... .......... .......... 50% 25.0M 6s
135000K .......... .......... .......... .......... .......... 50% 39.5M 6s
135050K .......... .......... .......... .......... .......... 50% 25.3M 6s
135100K .......... .......... .......... .......... .......... 50% 20.9M 6s
135150K .......... .......... .......... .......... .......... 50% 49.3M 6s
135200K .......... .......... .......... .......... .......... 50% 30.4M 6s
135250K .......... .......... .......... .......... .......... 50% 28.9M 6s
135300K .......... .......... .......... .......... .......... 50%  102M 6s
135350K .......... .......... .......... .......... .......... 50% 19.6M 6s
135400K .......... .......... .......... .......... .......... 50% 61.0M 6s
135450K .......... .......... .......... .......... .......... 50% 37.1M 6s
135500K .......... .......... .......... .......... .......... 50% 26.2M 6s
135550K .......... .......... .......... .......... .......... 51% 31.2M 6s
135600K .......... .......... .......... .......... .......... 51% 24.2M 6s
135650K .......... .......... .......... .......... .......... 51% 37.8M 6s
135700K .......... .......... .......... .......... .......... 51%  102M 6s
135750K .......... .......... .......... .......... .......... 51% 17.0M 6s
135800K .......... .......... .......... .......... .......... 51%  104M 6s
135850K .......... .......... .......... .......... .......... 51%  117M 6s
135900K .......... .......... .......... .......... .......... 51% 24.6M 6s
135950K .......... .......... .......... .......... .......... 51% 41.2M 6s
136000K .......... .......... .......... .......... .......... 51% 12.4M 6s
136050K .......... .......... .......... .......... .......... 51%  114M 6s
136100K .......... .......... .......... .......... .......... 51%  134M 6s
136150K .......... .......... .......... .......... .......... 51%  241M 6s
136200K .......... .......... .......... .......... .......... 51% 45.9M 6s
136250K .......... .......... .......... .......... .......... 51% 76.5M 6s
136300K .......... .......... .......... .......... .......... 51% 50.8M 6s
136350K .......... .......... .......... .......... .......... 51% 44.7M 6s
136400K .......... .......... .......... .......... .......... 51% 67.0M 6s
136450K .......... .......... .......... .......... .......... 51% 74.7M 6s
136500K .......... .......... .......... .......... .......... 51% 25.0M 6s
136550K .......... .......... .......... .......... .......... 51% 33.4M 6s
136600K .......... .......... .......... .......... .......... 51% 31.0M 6s
136650K .......... .......... .......... .......... .......... 51%  106M 6s
136700K .......... .......... .......... .......... .......... 51% 13.7M 6s
136750K .......... .......... .......... .......... .......... 51% 21.7M 6s
136800K .......... .......... .......... .......... .......... 51%  170M 6s
136850K .......... .......... .......... .......... .......... 51%  107M 6s
136900K .......... .......... .......... .......... .......... 51% 99.6M 6s
136950K .......... .......... .......... .......... .......... 51% 27.4M 6s
137000K .......... .......... .......... .......... .......... 51% 44.6M 6s
137050K .......... .......... .......... .......... .......... 51% 21.4M 6s
137100K .......... .......... .......... .......... .......... 51% 29.0M 6s
137150K .......... .......... .......... .......... .......... 51% 79.2M 6s
137200K .......... .......... .......... .......... .......... 51% 37.1M 6s
137250K .......... .......... .......... .......... .......... 51% 17.3M 6s
137300K .......... .......... .......... .......... .......... 51% 30.9M 6s
137350K .......... .......... .......... .......... .......... 51% 81.8M 6s
137400K .......... .......... .......... .......... .......... 51% 57.4M 6s
137450K .......... .......... .......... .......... .......... 51% 31.7M 6s
137500K .......... .......... .......... .......... .......... 51% 23.2M 6s
137550K .......... .......... .......... .......... .......... 51% 32.7M 6s
137600K .......... .......... .......... .......... .......... 51% 38.8M 6s
137650K .......... .......... .......... .......... .......... 51% 42.6M 6s
137700K .......... .......... .......... .......... .......... 51% 36.5M 6s
137750K .......... .......... .......... .......... .......... 51% 44.1M 6s
137800K .......... .......... .......... .......... .......... 51%  150M 6s
137850K .......... .......... .......... .......... .......... 51% 29.6M 6s
137900K .......... .......... .......... .......... .......... 51% 35.4M 6s
137950K .......... .......... .......... .......... .......... 51% 25.6M 6s
138000K .......... .......... .......... .......... .......... 51% 31.9M 6s
138050K .......... .......... .......... .......... .......... 51%  129M 6s
138100K .......... .......... .......... .......... .......... 51% 28.9M 6s
138150K .......... .......... .......... .......... .......... 51% 32.8M 6s
138200K .......... .......... .......... .......... .......... 52% 22.1M 6s
138250K .......... .......... .......... .......... .......... 52% 67.1M 6s
138300K .......... .......... .......... .......... .......... 52% 85.1M 6s
138350K .......... .......... .......... .......... .......... 52% 26.2M 6s
138400K .......... .......... .......... .......... .......... 52% 34.6M 6s
138450K .......... .......... .......... .......... .......... 52% 30.7M 6s
138500K .......... .......... .......... .......... .......... 52%  129M 6s
138550K .......... .......... .......... .......... .......... 52% 27.5M 6s
138600K .......... .......... .......... .......... .......... 52% 17.7M 6s
138650K .......... .......... .......... .......... .......... 52% 52.1M 6s
138700K .......... .......... .......... .......... .......... 52% 30.8M 6s
138750K .......... .......... .......... .......... .......... 52% 87.9M 6s
138800K .......... .......... .......... .......... .......... 52% 30.0M 6s
138850K .......... .......... .......... .......... .......... 52% 25.1M 6s
138900K .......... .......... .......... .......... .......... 52% 29.1M 6s
138950K .......... .......... .......... .......... .......... 52% 29.5M 6s
139000K .......... .......... .......... .......... .......... 52%  121M 6s
139050K .......... .......... .......... .......... .......... 52% 32.9M 6s
139100K .......... .......... .......... .......... .......... 52% 21.7M 6s
139150K .......... .......... .......... .......... .......... 52% 50.3M 6s
139200K .......... .......... .......... .......... .......... 52% 30.2M 6s
139250K .......... .......... .......... .......... .......... 52% 63.0M 6s
139300K .......... .......... .......... .......... .......... 52% 20.8M 6s
139350K .......... .......... .......... .......... .......... 52% 29.4M 6s
139400K .......... .......... .......... .......... .......... 52% 32.4M 6s
139450K .......... .......... .......... .......... .......... 52% 28.4M 6s
139500K .......... .......... .......... .......... .......... 52% 94.7M 6s
139550K .......... .......... .......... .......... .......... 52% 27.1M 6s
139600K .......... .......... .......... .......... .......... 52% 34.1M 6s
139650K .......... .......... .......... .......... .......... 52% 34.7M 6s
139700K .......... .......... .......... .......... .......... 52% 81.3M 6s
139750K .......... .......... .......... .......... .......... 52% 32.0M 6s
139800K .......... .......... .......... .......... .......... 52% 22.7M 6s
139850K .......... .......... .......... .......... .......... 52% 26.0M 6s
139900K .......... .......... .......... .......... .......... 52% 32.2M 6s
139950K .......... .......... .......... .......... .......... 52% 26.7M 6s
140000K .......... .......... .......... .......... .......... 52% 36.1M 6s
140050K .......... .......... .......... .......... .......... 52% 44.1M 6s
140100K .......... .......... .......... .......... .......... 52% 35.3M 6s
140150K .......... .......... .......... .......... .......... 52% 46.6M 6s
140200K .......... .......... .......... .......... .......... 52% 49.5M 6s
140250K .......... .......... .......... .......... .......... 52% 13.4M 6s
140300K .......... .......... .......... .......... .......... 52% 71.0M 6s
140350K .......... .......... .......... .......... .......... 52% 79.9M 6s
140400K .......... .......... .......... .......... .......... 52% 61.5M 6s
140450K .......... .......... .......... .......... .......... 52% 20.6M 6s
140500K .......... .......... .......... .......... .......... 52% 32.4M 6s
140550K .......... .......... .......... .......... .......... 52% 34.6M 6s
140600K .......... .......... .......... .......... .......... 52% 20.7M 6s
140650K .......... .......... .......... .......... .......... 52% 57.7M 6s
140700K .......... .......... .......... .......... .......... 52% 20.3M 6s
140750K .......... .......... .......... .......... .......... 52% 25.2M 6s
140800K .......... .......... .......... .......... .......... 52% 25.4M 6s
140850K .......... .......... .......... .......... .......... 53% 19.0M 6s
140900K .......... .......... .......... .......... .......... 53% 60.3M 6s
140950K .......... .......... .......... .......... .......... 53%  179M 6s
141000K .......... .......... .......... .......... .......... 53% 49.5M 6s
141050K .......... .......... .......... .......... .......... 53% 37.9M 6s
141100K .......... .......... .......... .......... .......... 53% 28.2M 6s
141150K .......... .......... .......... .......... .......... 53% 44.1M 6s
141200K .......... .......... .......... .......... .......... 53% 29.5M 6s
141250K .......... .......... .......... .......... .......... 53% 28.6M 6s
141300K .......... .......... .......... .......... .......... 53% 68.2M 6s
141350K .......... .......... .......... .......... .......... 53% 31.8M 6s
141400K .......... .......... .......... .......... .......... 53% 26.4M 6s
141450K .......... .......... .......... .......... .......... 53% 29.4M 6s
141500K .......... .......... .......... .......... .......... 53% 28.4M 6s
141550K .......... .......... .......... .......... .......... 53% 69.0M 6s
141600K .......... .......... .......... .......... .......... 53% 31.3M 6s
141650K .......... .......... .......... .......... .......... 53% 29.7M 6s
141700K .......... .......... .......... .......... .......... 53% 30.1M 6s
141750K .......... .......... .......... .......... .......... 53%  110M 6s
141800K .......... .......... .......... .......... .......... 53% 29.4M 6s
141850K .......... .......... .......... .......... .......... 53% 21.5M 6s
141900K .......... .......... .......... .......... .......... 53% 30.9M 6s
141950K .......... .......... .......... .......... .......... 53% 32.9M 6s
142000K .......... .......... .......... .......... .......... 53% 44.5M 6s
142050K .......... .......... .......... .......... .......... 53% 46.0M 6s
142100K .......... .......... .......... .......... .......... 53% 21.1M 6s
142150K .......... .......... .......... .......... .......... 53% 22.9M 6s
142200K .......... .......... .......... .......... .......... 53% 50.1M 6s
142250K .......... .......... .......... .......... .......... 53% 24.8M 6s
142300K .......... .......... .......... .......... .......... 53%  120M 6s
142350K .......... .......... .......... .......... .......... 53% 27.0M 6s
142400K .......... .......... .......... .......... .......... 53% 21.6M 6s
142450K .......... .......... .......... .......... .......... 53% 42.0M 6s
142500K .......... .......... .......... .......... .......... 53% 51.4M 6s
142550K .......... .......... .......... .......... .......... 53% 28.3M 6s
142600K .......... .......... .......... .......... .......... 53% 31.8M 6s
142650K .......... .......... .......... .......... .......... 53% 25.4M 6s
142700K .......... .......... .......... .......... .......... 53% 26.4M 6s
142750K .......... .......... .......... .......... .......... 53% 97.5M 6s
142800K .......... .......... .......... .......... .......... 53% 23.3M 6s
142850K .......... .......... .......... .......... .......... 53% 32.9M 6s
142900K .......... .......... .......... .......... .......... 53% 21.6M 6s
142950K .......... .......... .......... .......... .......... 53% 29.2M 6s
143000K .......... .......... .......... .......... .......... 53% 32.4M 6s
143050K .......... .......... .......... .......... .......... 53% 89.6M 6s
143100K .......... .......... .......... .......... .......... 53% 13.8M 6s
143150K .......... .......... .......... .......... .......... 53% 21.0M 6s
143200K .......... .......... .......... .......... .......... 53% 23.2M 6s
143250K .......... .......... .......... .......... .......... 53% 44.3M 6s
143300K .......... .......... .......... .......... .......... 53% 16.3M 6s
143350K .......... .......... .......... .......... .......... 53% 27.9M 6s
143400K .......... .......... .......... .......... .......... 53%  132M 6s
143450K .......... .......... .......... .......... .......... 53% 92.7M 6s
143500K .......... .......... .......... .......... .......... 54% 93.1M 6s
143550K .......... .......... .......... .......... .......... 54% 84.9M 6s
143600K .......... .......... .......... .......... .......... 54% 39.0M 6s
143650K .......... .......... .......... .......... .......... 54% 20.9M 6s
143700K .......... .......... .......... .......... .......... 54% 22.3M 6s
143750K .......... .......... .......... .......... .......... 54% 35.1M 6s
143800K .......... .......... .......... .......... .......... 54% 67.9M 6s
143850K .......... .......... .......... .......... .......... 54% 26.1M 6s
143900K .......... .......... .......... .......... .......... 54% 22.1M 6s
143950K .......... .......... .......... .......... .......... 54% 77.6M 6s
144000K .......... .......... .......... .......... .......... 54% 40.3M 6s
144050K .......... .......... .......... .......... .......... 54% 25.7M 6s
144100K .......... .......... .......... .......... .......... 54% 31.1M 6s
144150K .......... .......... .......... .......... .......... 54% 67.6M 6s
144200K .......... .......... .......... .......... .......... 54% 26.0M 6s
144250K .......... .......... .......... .......... .......... 54% 38.1M 6s
144300K .......... .......... .......... .......... .......... 54% 26.7M 6s
144350K .......... .......... .......... .......... .......... 54% 31.4M 6s
144400K .......... .......... .......... .......... .......... 54% 86.8M 6s
144450K .......... .......... .......... .......... .......... 54% 28.2M 6s
144500K .......... .......... .......... .......... .......... 54% 30.5M 6s
144550K .......... .......... .......... .......... .......... 54% 45.8M 6s
144600K .......... .......... .......... .......... .......... 54% 29.8M 6s
144650K .......... .......... .......... .......... .......... 54%  102M 6s
144700K .......... .......... .......... .......... .......... 54% 23.1M 6s
144750K .......... .......... .......... .......... .......... 54% 30.3M 6s
144800K .......... .......... .......... .......... .......... 54%  105M 6s
144850K .......... .......... .......... .......... .......... 54% 22.3M 6s
144900K .......... .......... .......... .......... .......... 54% 35.1M 6s
144950K .......... .......... .......... .......... .......... 54% 35.3M 6s
145000K .......... .......... .......... .......... .......... 54% 44.9M 6s
145050K .......... .......... .......... .......... .......... 54% 36.0M 6s
145100K .......... .......... .......... .......... .......... 54% 18.9M 6s
145150K .......... .......... .......... .......... .......... 54% 49.2M 6s
145200K .......... .......... .......... .......... .......... 54% 24.1M 6s
145250K .......... .......... .......... .......... .......... 54% 27.0M 6s
145300K .......... .......... .......... .......... .......... 54% 36.5M 6s
145350K .......... .......... .......... .......... .......... 54% 28.3M 6s
145400K .......... .......... .......... .......... .......... 54% 37.1M 6s
145450K .......... .......... .......... .......... .......... 54% 34.0M 6s
145500K .......... .......... .......... .......... .......... 54% 32.9M 6s
145550K .......... .......... .......... .......... .......... 54% 46.5M 6s
145600K .......... .......... .......... .......... .......... 54% 22.4M 6s
145650K .......... .......... .......... .......... .......... 54% 31.6M 6s
145700K .......... .......... .......... .......... .......... 54% 37.9M 6s
145750K .......... .......... .......... .......... .......... 54% 54.1M 6s
145800K .......... .......... .......... .......... .......... 54% 40.8M 6s
145850K .......... .......... .......... .......... .......... 54% 23.9M 6s
145900K .......... .......... .......... .......... .......... 54% 30.0M 6s
145950K .......... .......... .......... .......... .......... 54% 24.3M 6s
146000K .......... .......... .......... .......... .......... 54% 22.3M 6s
146050K .......... .......... .......... .......... .......... 54% 41.3M 6s
146100K .......... .......... .......... .......... .......... 54% 32.9M 6s
146150K .......... .......... .......... .......... .......... 55% 39.8M 6s
146200K .......... .......... .......... .......... .......... 55% 33.2M 6s
146250K .......... .......... .......... .......... .......... 55% 54.2M 6s
146300K .......... .......... .......... .......... .......... 55% 19.7M 6s
146350K .......... .......... .......... .......... .......... 55% 15.5M 6s
146400K .......... .......... .......... .......... .......... 55% 23.2M 6s
146450K .......... .......... .......... .......... .......... 55% 15.8M 6s
146500K .......... .......... .......... .......... .......... 55% 33.2M 6s
146550K .......... .......... .......... .......... .......... 55% 18.1M 6s
146600K .......... .......... .......... .......... .......... 55% 19.1M 6s
146650K .......... .......... .......... .......... .......... 55% 28.2M 6s
146700K .......... .......... .......... .......... .......... 55% 36.2M 6s
146750K .......... .......... .......... .......... .......... 55%  104M 6s
146800K .......... .......... .......... .......... .......... 55% 95.3M 6s
146850K .......... .......... .......... .......... .......... 55%  116M 6s
146900K .......... .......... .......... .......... .......... 55%  143M 6s
146950K .......... .......... .......... .......... .......... 55% 96.1M 5s
147000K .......... .......... .......... .......... .......... 55% 70.5M 5s
147050K .......... .......... .......... .......... .......... 55%  130M 5s
147100K .......... .......... .......... .......... .......... 55% 31.6M 5s
147150K .......... .......... .......... .......... .......... 55% 17.8M 5s
147200K .......... .......... .......... .......... .......... 55% 36.2M 5s
147250K .......... .......... .......... .......... .......... 55%  152M 5s
147300K .......... .......... .......... .......... .......... 55% 30.2M 5s
147350K .......... .......... .......... .......... .......... 55% 26.0M 5s
147400K .......... .......... .......... .......... .......... 55% 95.2M 5s
147450K .......... .......... .......... .......... .......... 55% 23.2M 5s
147500K .......... .......... .......... .......... .......... 55% 25.6M 5s
147550K .......... .......... .......... .......... .......... 55% 14.1M 5s
147600K .......... .......... .......... .......... .......... 55%  134M 5s
147650K .......... .......... .......... .......... .......... 55% 34.6M 5s
147700K .......... .......... .......... .......... .......... 55% 23.1M 5s
147750K .......... .......... .......... .......... .......... 55%  127M 5s
147800K .......... .......... .......... .......... .......... 55% 27.1M 5s
147850K .......... .......... .......... .......... .......... 55% 34.0M 5s
147900K .......... .......... .......... .......... .......... 55% 32.6M 5s
147950K .......... .......... .......... .......... .......... 55% 30.4M 5s
148000K .......... .......... .......... .......... .......... 55% 35.3M 5s
148050K .......... .......... .......... .......... .......... 55% 24.7M 5s
148100K .......... .......... .......... .......... .......... 55% 33.9M 5s
148150K .......... .......... .......... .......... .......... 55% 28.2M 5s
148200K .......... .......... .......... .......... .......... 55% 73.1M 5s
148250K .......... .......... .......... .......... .......... 55% 34.5M 5s
148300K .......... .......... .......... .......... .......... 55% 34.2M 5s
148350K .......... .......... .......... .......... .......... 55% 29.4M 5s
148400K .......... .......... .......... .......... .......... 55% 33.5M 5s
148450K .......... .......... .......... .......... .......... 55% 59.8M 5s
148500K .......... .......... .......... .......... .......... 55% 38.9M 5s
148550K .......... .......... .......... .......... .......... 55% 27.1M 5s
148600K .......... .......... .......... .......... .......... 55% 30.7M 5s
148650K .......... .......... .......... .......... .......... 55% 45.6M 5s
148700K .......... .......... .......... .......... .......... 55% 13.8M 5s
148750K .......... .......... .......... .......... .......... 55% 39.4M 5s
148800K .......... .......... .......... .......... .......... 55%  131M 5s
148850K .......... .......... .......... .......... .......... 56% 85.9M 5s
148900K .......... .......... .......... .......... .......... 56% 83.4M 5s
148950K .......... .......... .......... .......... .......... 56% 35.8M 5s
149000K .......... .......... .......... .......... .......... 56% 12.7M 5s
149050K .......... .......... .......... .......... .......... 56% 36.3M 5s
149100K .......... .......... .......... .......... .......... 56% 13.8M 5s
149150K .......... .......... .......... .......... .......... 56%  106M 5s
149200K .......... .......... .......... .......... .......... 56% 98.0M 5s
149250K .......... .......... .......... .......... .......... 56%  121M 5s
149300K .......... .......... .......... .......... .......... 56% 22.2M 5s
149350K .......... .......... .......... .......... .......... 56%  109M 5s
149400K .......... .......... .......... .......... .......... 56% 18.2M 5s
149450K .......... .......... .......... .......... .......... 56% 32.9M 5s
149500K .......... .......... .......... .......... .......... 56% 16.0M 5s
149550K .......... .......... .......... .......... .......... 56%  158M 5s
149600K .......... .......... .......... .......... .......... 56% 47.2M 5s
149650K .......... .......... .......... .......... .......... 56% 62.2M 5s
149700K .......... .......... .......... .......... .......... 56% 28.2M 5s
149750K .......... .......... .......... .......... .......... 56% 35.2M 5s
149800K .......... .......... .......... .......... .......... 56% 57.1M 5s
149850K .......... .......... .......... .......... .......... 56% 40.5M 5s
149900K .......... .......... .......... .......... .......... 56% 30.4M 5s
149950K .......... .......... .......... .......... .......... 56% 21.1M 5s
150000K .......... .......... .......... .......... .......... 56% 60.6M 5s
150050K .......... .......... .......... .......... .......... 56% 89.0M 5s
150100K .......... .......... .......... .......... .......... 56% 31.9M 5s
150150K .......... .......... .......... .......... .......... 56% 33.1M 5s
150200K .......... .......... .......... .......... .......... 56% 26.5M 5s
150250K .......... .......... .......... .......... .......... 56% 33.7M 5s
150300K .......... .......... .......... .......... .......... 56% 52.7M 5s
150350K .......... .......... .......... .......... .......... 56% 27.0M 5s
150400K .......... .......... .......... .......... .......... 56% 34.0M 5s
150450K .......... .......... .......... .......... .......... 56% 29.3M 5s
150500K .......... .......... .......... .......... .......... 56% 32.6M 5s
150550K .......... .......... .......... .......... .......... 56% 91.8M 5s
150600K .......... .......... .......... .......... .......... 56% 28.1M 5s
150650K .......... .......... .......... .......... .......... 56% 32.6M 5s
150700K .......... .......... .......... .......... .......... 56% 30.6M 5s
150750K .......... .......... .......... .......... .......... 56% 31.0M 5s
150800K .......... .......... .......... .......... .......... 56% 43.9M 5s
150850K .......... .......... .......... .......... .......... 56% 32.8M 5s
150900K .......... .......... .......... .......... .......... 56% 29.7M 5s
150950K .......... .......... .......... .......... .......... 56% 45.4M 5s
151000K .......... .......... .......... .......... .......... 56% 51.1M 5s
151050K .......... .......... .......... .......... .......... 56% 29.6M 5s
151100K .......... .......... .......... .......... .......... 56% 31.6M 5s
151150K .......... .......... .......... .......... .......... 56% 29.6M 5s
151200K .......... .......... .......... .......... .......... 56% 29.9M 5s
151250K .......... .......... .......... .......... .......... 56%  106M 5s
151300K .......... .......... .......... .......... .......... 56% 33.1M 5s
151350K .......... .......... .......... .......... .......... 56% 27.2M 5s
151400K .......... .......... .......... .......... .......... 56% 24.4M 5s
151450K .......... .......... .......... .......... .......... 56% 35.5M 5s
151500K .......... .......... .......... .......... .......... 57% 24.8M 5s
151550K .......... .......... .......... .......... .......... 57% 48.7M 5s
151600K .......... .......... .......... .......... .......... 57% 19.1M 5s
151650K .......... .......... .......... .......... .......... 57% 56.2M 5s
151700K .......... .......... .......... .......... .......... 57% 28.3M 5s
151750K .......... .......... .......... .......... .......... 57% 44.4M 5s
151800K .......... .......... .......... .......... .......... 57%  195M 5s
151850K .......... .......... .......... .......... .......... 57% 14.1M 5s
151900K .......... .......... .......... .......... .......... 57% 97.3M 5s
151950K .......... .......... .......... .......... .......... 57% 92.1M 5s
152000K .......... .......... .......... .......... .......... 57% 91.9M 5s
152050K .......... .......... .......... .......... .......... 57% 28.2M 5s
152100K .......... .......... .......... .......... .......... 57% 17.8M 5s
152150K .......... .......... .......... .......... .......... 57% 33.4M 5s
152200K .......... .......... .......... .......... .......... 57% 42.7M 5s
152250K .......... .......... .......... .......... .......... 57% 48.0M 5s
152300K .......... .......... .......... .......... .......... 57%  122M 5s
152350K .......... .......... .......... .......... .......... 57% 17.5M 5s
152400K .......... .......... .......... .......... .......... 57% 81.4M 5s
152450K .......... .......... .......... .......... .......... 57% 28.9M 5s
152500K .......... .......... .......... .......... .......... 57%  129M 5s
152550K .......... .......... .......... .......... .......... 57% 44.6M 5s
152600K .......... .......... .......... .......... .......... 57% 44.9M 5s
152650K .......... .......... .......... .......... .......... 57% 92.4M 5s
152700K .......... .......... .......... .......... .......... 57% 26.4M 5s
152750K .......... .......... .......... .......... .......... 57% 32.3M 5s
152800K .......... .......... .......... .......... .......... 57% 33.1M 5s
152850K .......... .......... .......... .......... .......... 57% 34.5M 5s
152900K .......... .......... .......... .......... .......... 57% 75.7M 5s
152950K .......... .......... .......... .......... .......... 57% 16.2M 5s
153000K .......... .......... .......... .......... .......... 57% 98.7M 5s
153050K .......... .......... .......... .......... .......... 57% 34.1M 5s
153100K .......... .......... .......... .......... .......... 57% 35.2M 5s
153150K .......... .......... .......... .......... .......... 57%  107M 5s
153200K .......... .......... .......... .......... .......... 57% 29.0M 5s
153250K .......... .......... .......... .......... .......... 57% 34.5M 5s
153300K .......... .......... .......... .......... .......... 57% 33.0M 5s
153350K .......... .......... .......... .......... .......... 57% 65.9M 5s
153400K .......... .......... .......... .......... .......... 57% 18.5M 5s
153450K .......... .......... .......... .......... .......... 57% 46.5M 5s
153500K .......... .......... .......... .......... .......... 57% 44.4M 5s
153550K .......... .......... .......... .......... .......... 57% 32.6M 5s
153600K .......... .......... .......... .......... .......... 57% 70.2M 5s
153650K .......... .......... .......... .......... .......... 57% 35.9M 5s
153700K .......... .......... .......... .......... .......... 57% 19.4M 5s
153750K .......... .......... .......... .......... .......... 57% 42.4M 5s
153800K .......... .......... .......... .......... .......... 57% 47.0M 5s
153850K .......... .......... .......... .......... .......... 57% 43.0M 5s
153900K .......... .......... .......... .......... .......... 57% 46.3M 5s
153950K .......... .......... .......... .......... .......... 57% 28.0M 5s
154000K .......... .......... .......... .......... .......... 57% 24.7M 5s
154050K .......... .......... .......... .......... .......... 57% 63.0M 5s
154100K .......... .......... .......... .......... .......... 57% 28.9M 5s
154150K .......... .......... .......... .......... .......... 58% 38.3M 5s
154200K .......... .......... .......... .......... .......... 58% 32.1M 5s
154250K .......... .......... .......... .......... .......... 58% 66.9M 5s
154300K .......... .......... .......... .......... .......... 58% 22.8M 5s
154350K .......... .......... .......... .......... .......... 58% 87.8M 5s
154400K .......... .......... .......... .......... .......... 58% 38.1M 5s
154450K .......... .......... .......... .......... .......... 58% 33.4M 5s
154500K .......... .......... .......... .......... .......... 58% 31.5M 5s
154550K .......... .......... .......... .......... .......... 58% 86.8M 5s
154600K .......... .......... .......... .......... .......... 58% 27.7M 5s
154650K .......... .......... .......... .......... .......... 58% 24.6M 5s
154700K .......... .......... .......... .......... .......... 58% 17.8M 5s
154750K .......... .......... .......... .......... .......... 58% 46.7M 5s
154800K .......... .......... .......... .......... .......... 58% 51.6M 5s
154850K .......... .......... .......... .......... .......... 58% 79.2M 5s
154900K .......... .......... .......... .......... .......... 58% 28.5M 5s
154950K .......... .......... .......... .......... .......... 58% 32.2M 5s
155000K .......... .......... .......... .......... .......... 58%  138M 5s
155050K .......... .......... .......... .......... .......... 58% 44.0M 5s
155100K .......... .......... .......... .......... .......... 58% 30.3M 5s
155150K .......... .......... .......... .......... .......... 58% 34.4M 5s
155200K .......... .......... .......... .......... .......... 58% 32.1M 5s
155250K .......... .......... .......... .......... .......... 58% 68.7M 5s
155300K .......... .......... .......... .......... .......... 58% 32.5M 5s
155350K .......... .......... .......... .......... .......... 58% 30.6M 5s
155400K .......... .......... .......... .......... .......... 58% 37.2M 5s
155450K .......... .......... .......... .......... .......... 58% 27.4M 5s
155500K .......... .......... .......... .......... .......... 58%  106M 5s
155550K .......... .......... .......... .......... .......... 58% 30.4M 5s
155600K .......... .......... .......... .......... .......... 58% 32.5M 5s
155650K .......... .......... .......... .......... .......... 58% 31.4M 5s
155700K .......... .......... .......... .......... .......... 58% 31.6M 5s
155750K .......... .......... .......... .......... .......... 58% 71.4M 5s
155800K .......... .......... .......... .......... .......... 58% 15.9M 5s
155850K .......... .......... .......... .......... .......... 58% 60.7M 5s
155900K .......... .......... .......... .......... .......... 58% 65.2M 5s
155950K .......... .......... .......... .......... .......... 58% 55.2M 5s
156000K .......... .......... .......... .......... .......... 58% 18.1M 5s
156050K .......... .......... .......... .......... .......... 58% 56.2M 5s
156100K .......... .......... .......... .......... .......... 58% 37.1M 5s
156150K .......... .......... .......... .......... .......... 58% 19.7M 5s
156200K .......... .......... .......... .......... .......... 58% 37.8M 5s
156250K .......... .......... .......... .......... .......... 58% 30.3M 5s
156300K .......... .......... .......... .......... .......... 58%  177M 5s
156350K .......... .......... .......... .......... .......... 58% 42.3M 5s
156400K .......... .......... .......... .......... .......... 58% 96.4M 5s
156450K .......... .......... .......... .......... .......... 58% 23.0M 5s
156500K .......... .......... .......... .......... .......... 58% 56.6M 5s
156550K .......... .......... .......... .......... .......... 58% 16.3M 5s
156600K .......... .......... .......... .......... .......... 58% 90.9M 5s
156650K .......... .......... .......... .......... .......... 58%  120M 5s
156700K .......... .......... .......... .......... .......... 58% 33.0M 5s
156750K .......... .......... .......... .......... .......... 58% 10.8M 5s
156800K .......... .......... .......... .......... .......... 59%  137M 5s
156850K .......... .......... .......... .......... .......... 59% 47.0M 5s
156900K .......... .......... .......... .......... .......... 59%  134M 5s
156950K .......... .......... .......... .......... .......... 59% 68.6M 5s
157000K .......... .......... .......... .......... .......... 59% 29.1M 5s
157050K .......... .......... .......... .......... .......... 59% 7.16M 5s
157100K .......... .......... .......... .......... .......... 59%  116M 5s
157150K .......... .......... .......... .......... .......... 59% 61.8M 5s
157200K .......... .......... .......... .......... .......... 59%  131M 5s
157250K .......... .......... .......... .......... .......... 59% 89.8M 5s
157300K .......... .......... .......... .......... .......... 59%  119M 5s
157350K .......... .......... .......... .......... .......... 59% 68.1M 5s
157400K .......... .......... .......... .......... .......... 59% 50.3M 5s
157450K .......... .......... .......... .......... .......... 59% 26.0M 5s
157500K .......... .......... .......... .......... .......... 59% 19.4M 5s
157550K .......... .......... .......... .......... .......... 59% 18.4M 5s
157600K .......... .......... .......... .......... .......... 59% 93.4M 5s
157650K .......... .......... .......... .......... .......... 59% 58.4M 5s
157700K .......... .......... .......... .......... .......... 59% 31.9M 5s
157750K .......... .......... .......... .......... .......... 59% 20.5M 5s
157800K .......... .......... .......... .......... .......... 59% 72.1M 5s
157850K .......... .......... .......... .......... .......... 59% 19.9M 5s
157900K .......... .......... .......... .......... .......... 59% 28.6M 5s
157950K .......... .......... .......... .......... .......... 59% 22.1M 5s
158000K .......... .......... .......... .......... .......... 59% 15.6M 5s
158050K .......... .......... .......... .......... .......... 59%  125M 5s
158100K .......... .......... .......... .......... .......... 59%  129M 5s
158150K .......... .......... .......... .......... .......... 59% 33.3M 5s
158200K .......... .......... .......... .......... .......... 59% 19.1M 5s
158250K .......... .......... .......... .......... .......... 59% 73.2M 5s
158300K .......... .......... .......... .......... .......... 59% 48.5M 5s
158350K .......... .......... .......... .......... .......... 59% 15.4M 5s
158400K .......... .......... .......... .......... .......... 59% 47.7M 5s
158450K .......... .......... .......... .......... .......... 59% 36.1M 5s
158500K .......... .......... .......... .......... .......... 59% 12.5M 5s
158550K .......... .......... .......... .......... .......... 59% 88.6M 5s
158600K .......... .......... .......... .......... .......... 59%  243M 5s
158650K .......... .......... .......... .......... .......... 59% 19.2M 5s
158700K .......... .......... .......... .......... .......... 59% 47.1M 5s
158750K .......... .......... .......... .......... .......... 59% 95.7M 5s
158800K .......... .......... .......... .......... .......... 59% 22.2M 5s
158850K .......... .......... .......... .......... .......... 59% 21.9M 5s
158900K .......... .......... .......... .......... .......... 59% 59.4M 5s
158950K .......... .......... .......... .......... .......... 59% 22.6M 5s
159000K .......... .......... .......... .......... .......... 59% 27.5M 5s
159050K .......... .......... .......... .......... .......... 59% 63.1M 5s
159100K .......... .......... .......... .......... .......... 59% 21.6M 5s
159150K .......... .......... .......... .......... .......... 59% 22.6M 5s
159200K .......... .......... .......... .......... .......... 59% 64.7M 5s
159250K .......... .......... .......... .......... .......... 59% 27.7M 5s
159300K .......... .......... .......... .......... .......... 59% 21.0M 5s
159350K .......... .......... .......... .......... .......... 59% 26.9M 5s
159400K .......... .......... .......... .......... .......... 59% 27.5M 5s
159450K .......... .......... .......... .......... .......... 60% 35.5M 5s
159500K .......... .......... .......... .......... .......... 60% 30.4M 5s
159550K .......... .......... .......... .......... .......... 60% 28.1M 5s
159600K .......... .......... .......... .......... .......... 60% 38.3M 5s
159650K .......... .......... .......... .......... .......... 60% 21.2M 5s
159700K .......... .......... .......... .......... .......... 60% 30.5M 5s
159750K .......... .......... .......... .......... .......... 60% 42.8M 5s
159800K .......... .......... .......... .......... .......... 60% 15.1M 5s
159850K .......... .......... .......... .......... .......... 60% 22.1M 5s
159900K .......... .......... .......... .......... .......... 60% 36.2M 5s
159950K .......... .......... .......... .......... .......... 60% 38.8M 5s
160000K .......... .......... .......... .......... .......... 60% 35.6M 5s
160050K .......... .......... .......... .......... .......... 60% 37.9M 5s
160100K .......... .......... .......... .......... .......... 60% 20.9M 5s
160150K .......... .......... .......... .......... .......... 60% 58.3M 5s
160200K .......... .......... .......... .......... .......... 60% 37.2M 5s
160250K .......... .......... .......... .......... .......... 60% 18.1M 5s
160300K .......... .......... .......... .......... .......... 60% 40.7M 5s
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160400K .......... .......... .......... .......... .......... 60% 15.7M 5s
160450K .......... .......... .......... .......... .......... 60% 60.1M 5s
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160650K .......... .......... .......... .......... .......... 60% 70.9M 5s
160700K .......... .......... .......... .......... .......... 60% 13.1M 5s
160750K .......... .......... .......... .......... .......... 60% 79.2M 5s
160800K .......... .......... .......... .......... .......... 60% 33.2M 5s
160850K .......... .......... .......... .......... .......... 60% 48.9M 5s
160900K .......... .......... .......... .......... .......... 60% 17.2M 5s
160950K .......... .......... .......... .......... .......... 60% 26.0M 5s
161000K .......... .......... .......... .......... .......... 60% 66.8M 5s
161050K .......... .......... .......... .......... .......... 60% 19.9M 5s
161100K .......... .......... .......... .......... .......... 60% 58.3M 5s
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161200K .......... .......... .......... .......... .......... 60% 21.3M 5s
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161350K .......... .......... .......... .......... .......... 60% 24.1M 5s
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161500K .......... .......... .......... .......... .......... 60% 24.6M 5s
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161600K .......... .......... .......... .......... .......... 60% 44.4M 5s
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161750K .......... .......... .......... .......... .......... 60% 32.9M 5s
161800K .......... .......... .......... .......... .......... 60% 41.4M 5s
161850K .......... .......... .......... .......... .......... 60% 19.2M 5s
161900K .......... .......... .......... .......... .......... 60% 45.3M 5s
161950K .......... .......... .......... .......... .......... 60% 32.6M 5s
162000K .......... .......... .......... .......... .......... 60% 14.4M 5s
162050K .......... .......... .......... .......... .......... 60%  119M 5s
162100K .......... .......... .......... .......... .......... 61% 43.8M 5s
162150K .......... .......... .......... .......... .......... 61% 13.9M 5s
162200K .......... .......... .......... .......... .......... 61% 44.1M 5s
162250K .......... .......... .......... .......... .......... 61% 98.9M 5s
162300K .......... .......... .......... .......... .......... 61% 17.8M 5s
162350K .......... .......... .......... .......... .......... 61% 21.2M 5s
162400K .......... .......... .......... .......... .......... 61% 78.9M 5s
162450K .......... .......... .......... .......... .......... 61% 18.9M 5s
162500K .......... .......... .......... .......... .......... 61% 31.3M 5s
162550K .......... .......... .......... .......... .......... 61% 76.5M 5s
162600K .......... .......... .......... .......... .......... 61% 43.3M 5s
162650K .......... .......... .......... .......... .......... 61% 16.7M 5s
162700K .......... .......... .......... .......... .......... 61% 31.0M 5s
162750K .......... .......... .......... .......... .......... 61% 74.0M 5s
162800K .......... .......... .......... .......... .......... 61% 15.2M 5s
162850K .......... .......... .......... .......... .......... 61% 42.7M 5s
162900K .......... .......... .......... .......... .......... 61% 41.7M 5s
162950K .......... .......... .......... .......... .......... 61% 27.3M 5s
163000K .......... .......... .......... .......... .......... 61% 22.1M 5s
163050K .......... .......... .......... .......... .......... 61% 79.5M 5s
163100K .......... .......... .......... .......... .......... 61% 39.9M 5s
163150K .......... .......... .......... .......... .......... 61% 15.2M 5s
163200K .......... .......... .......... .......... .......... 61% 40.6M 5s
163250K .......... .......... .......... .......... .......... 61% 84.3M 5s
163300K .......... .......... .......... .......... .......... 61% 25.0M 5s
163350K .......... .......... .......... .......... .......... 61% 22.6M 5s
163400K .......... .......... .......... .......... .......... 61% 38.7M 5s
163450K .......... .......... .......... .......... .......... 61% 47.2M 5s
163500K .......... .......... .......... .......... .......... 61% 26.1M 5s
163550K .......... .......... .......... .......... .......... 61% 27.9M 5s
163600K .......... .......... .......... .......... .......... 61% 25.5M 5s
163650K .......... .......... .......... .......... .......... 61% 47.0M 5s
163700K .......... .......... .......... .......... .......... 61% 17.8M 5s
163750K .......... .......... .......... .......... .......... 61% 48.2M 5s
163800K .......... .......... .......... .......... .......... 61% 25.9M 5s
163850K .......... .......... .......... .......... .......... 61% 31.5M 5s
163900K .......... .......... .......... .......... .......... 61% 37.1M 5s
163950K .......... .......... .......... .......... .......... 61% 77.1M 5s
164000K .......... .......... .......... .......... .......... 61% 81.3M 5s
164050K .......... .......... .......... .......... .......... 61% 14.9M 5s
164100K .......... .......... .......... .......... .......... 61% 43.9M 5s
164150K .......... .......... .......... .......... .......... 61% 61.2M 5s
164200K .......... .......... .......... .......... .......... 61% 12.8M 5s
164250K .......... .......... .......... .......... .......... 61%  162M 5s
164300K .......... .......... .......... .......... .......... 61% 30.9M 5s
164350K .......... .......... .......... .......... .......... 61% 17.8M 5s
164400K .......... .......... .......... .......... .......... 61% 67.0M 5s
164450K .......... .......... .......... .......... .......... 61% 35.1M 5s
164500K .......... .......... .......... .......... .......... 61% 14.7M 5s
164550K .......... .......... .......... .......... .......... 61% 21.8M 5s
164600K .......... .......... .......... .......... .......... 61% 45.2M 5s
164650K .......... .......... .......... .......... .......... 61% 36.5M 5s
164700K .......... .......... .......... .......... .......... 61% 40.3M 5s
164750K .......... .......... .......... .......... .......... 61% 33.9M 4s
164800K .......... .......... .......... .......... .......... 62% 23.3M 4s
164850K .......... .......... .......... .......... .......... 62% 27.5M 4s
164900K .......... .......... .......... .......... .......... 62% 47.7M 4s
164950K .......... .......... .......... .......... .......... 62% 44.3M 4s
165000K .......... .......... .......... .......... .......... 62% 17.7M 4s
165050K .......... .......... .......... .......... .......... 62% 35.8M 4s
165100K .......... .......... .......... .......... .......... 62% 35.0M 4s
165150K .......... .......... .......... .......... .......... 62% 20.6M 4s
165200K .......... .......... .......... .......... .......... 62% 26.6M 4s
165250K .......... .......... .......... .......... .......... 62% 39.1M 4s
165300K .......... .......... .......... .......... .......... 62% 20.6M 4s
165350K .......... .......... .......... .......... .......... 62% 30.4M 4s
165400K .......... .......... .......... .......... .......... 62% 39.5M 4s
165450K .......... .......... .......... .......... .......... 62% 28.4M 4s
165500K .......... .......... .......... .......... .......... 62% 24.7M 4s
165550K .......... .......... .......... .......... .......... 62% 68.6M 4s
165600K .......... .......... .......... .......... .......... 62% 22.6M 4s
165650K .......... .......... .......... .......... .......... 62% 21.0M 4s
165700K .......... .......... .......... .......... .......... 62% 46.0M 4s
165750K .......... .......... .......... .......... .......... 62% 28.3M 4s
165800K .......... .......... .......... .......... .......... 62% 29.4M 4s
165850K .......... .......... .......... .......... .......... 62% 26.3M 4s
165900K .......... .......... .......... .......... .......... 62% 37.8M 4s
165950K .......... .......... .......... .......... .......... 62% 32.0M 4s
166000K .......... .......... .......... .......... .......... 62% 23.6M 4s
166050K .......... .......... .......... .......... .......... 62% 79.4M 4s
166100K .......... .......... .......... .......... .......... 62% 19.4M 4s
166150K .......... .......... .......... .......... .......... 62% 61.9M 4s
166200K .......... .......... .......... .......... .......... 62% 23.0M 4s
166250K .......... .......... .......... .......... .......... 62% 25.9M 4s
166300K .......... .......... .......... .......... .......... 62% 72.7M 4s
166350K .......... .......... .......... .......... .......... 62% 28.2M 4s
166400K .......... .......... .......... .......... .......... 62% 36.1M 4s
166450K .......... .......... .......... .......... .......... 62% 34.3M 4s
166500K .......... .......... .......... .......... .......... 62% 30.8M 4s
166550K .......... .......... .......... .......... .......... 62% 25.7M 4s
166600K .......... .......... .......... .......... .......... 62% 22.2M 4s
166650K .......... .......... .......... .......... .......... 62% 93.1M 4s
166700K .......... .......... .......... .......... .......... 62% 26.2M 4s
166750K .......... .......... .......... .......... .......... 62% 48.5M 4s
166800K .......... .......... .......... .......... .......... 62% 20.8M 4s
166850K .......... .......... .......... .......... .......... 62% 58.7M 4s
166900K .......... .......... .......... .......... .......... 62% 29.4M 4s
166950K .......... .......... .......... .......... .......... 62% 22.1M 4s
167000K .......... .......... .......... .......... .......... 62% 36.0M 4s
167050K .......... .......... .......... .......... .......... 62% 83.7M 4s
167100K .......... .......... .......... .......... .......... 62% 31.3M 4s
167150K .......... .......... .......... .......... .......... 62% 22.4M 4s
167200K .......... .......... .......... .......... .......... 62% 36.0M 4s
167250K .......... .......... .......... .......... .......... 62% 37.7M 4s
167300K .......... .......... .......... .......... .......... 62% 43.8M 4s
167350K .......... .......... .......... .......... .......... 62% 17.6M 4s
167400K .......... .......... .......... .......... .......... 62% 62.5M 4s
167450K .......... .......... .......... .......... .......... 63% 33.0M 4s
167500K .......... .......... .......... .......... .......... 63% 26.0M 4s
167550K .......... .......... .......... .......... .......... 63% 27.3M 4s
167600K .......... .......... .......... .......... .......... 63% 19.9M 4s
167650K .......... .......... .......... .......... .......... 63% 53.9M 4s
167700K .......... .......... .......... .......... .......... 63% 21.0M 4s
167750K .......... .......... .......... .......... .......... 63%  170M 4s
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167850K .......... .......... .......... .......... .......... 63%  144M 4s
167900K .......... .......... .......... .......... .......... 63%  197M 4s
167950K .......... .......... .......... .......... .......... 63%  111M 4s
168000K .......... .......... .......... .......... .......... 63%  147M 4s
168050K .......... .......... .......... .......... .......... 63% 25.4M 4s
168100K .......... .......... .......... .......... .......... 63% 29.1M 4s
168150K .......... .......... .......... .......... .......... 63% 51.6M 4s
168200K .......... .......... .......... .......... .......... 63% 35.3M 4s
168250K .......... .......... .......... .......... .......... 63% 15.8M 4s
168300K .......... .......... .......... .......... .......... 63% 23.1M 4s
168350K .......... .......... .......... .......... .......... 63% 65.3M 4s
168400K .......... .......... .......... .......... .......... 63% 21.6M 4s
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168650K .......... .......... .......... .......... .......... 63%  197M 4s
168700K .......... .......... .......... .......... .......... 63%  123M 4s
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168900K .......... .......... .......... .......... .......... 63%  147M 4s
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169000K .......... .......... .......... .......... .......... 63% 37.9M 4s
169050K .......... .......... .......... .......... .......... 63% 67.4M 4s
169100K .......... .......... .......... .......... .......... 63%  102M 4s
169150K .......... .......... .......... .......... .......... 63% 52.6M 4s
169200K .......... .......... .......... .......... .......... 63% 29.5M 4s
169250K .......... .......... .......... .......... .......... 63% 41.2M 4s
169300K .......... .......... .......... .......... .......... 63% 89.1M 4s
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170000K .......... .......... .......... .......... .......... 63% 79.2M 4s
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170100K .......... .......... .......... .......... .......... 64% 55.3M 4s
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170200K .......... .......... .......... .......... .......... 64% 35.4M 4s
170250K .......... .......... .......... .......... .......... 64% 72.7M 4s
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170900K .......... .......... .......... .......... .......... 64% 53.9M 4s
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171000K .......... .......... .......... .......... .......... 64%  114M 4s
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171100K .......... .......... .......... .......... .......... 64% 37.8M 4s
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171500K .......... .......... .......... .......... .......... 64% 90.2M 4s
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171600K .......... .......... .......... .......... .......... 64% 62.1M 4s
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171700K .......... .......... .......... .......... .......... 64% 81.9M 4s
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172000K .......... .......... .......... .......... .......... 64% 14.6M 4s
172050K .......... .......... .......... .......... .......... 64% 24.2M 4s
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172150K .......... .......... .......... .......... .......... 64% 49.0M 4s
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172250K .......... .......... .......... .......... .......... 64% 45.2M 4s
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172400K .......... .......... .......... .......... .......... 64% 91.4M 4s
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172500K .......... .......... .......... .......... .......... 64%  157M 4s
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172800K .......... .......... .......... .......... .......... 65%  189M 4s
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173000K .......... .......... .......... .......... .......... 65% 31.5M 4s
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173100K .......... .......... .......... .......... .......... 65% 22.4M 4s
173150K .......... .......... .......... .......... .......... 65% 36.3M 4s
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173250K .......... .......... .......... .......... .......... 65% 40.6M 4s
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173850K .......... .......... .......... .......... .......... 65% 89.6M 4s
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174000K .......... .......... .......... .......... .......... 65% 64.4M 4s
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174100K .......... .......... .......... .......... .......... 65% 20.7M 4s
174150K .......... .......... .......... .......... .......... 65% 31.5M 4s
174200K .......... .......... .......... .......... .......... 65% 46.2M 4s
174250K .......... .......... .......... .......... .......... 65%  127M 4s
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174400K .......... .......... .......... .......... .......... 65% 81.6M 4s
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175000K .......... .......... .......... .......... .......... 65% 43.9M 4s
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179100K .......... .......... .......... .......... .......... 67% 45.7M 4s
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180000K .......... .......... .......... .......... .......... 67%  106M 4s
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180100K .......... .......... .......... .......... .......... 67% 92.1M 4s
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180750K .......... .......... .......... .......... .......... 68% 92.7M 4s
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180850K .......... .......... .......... .......... .......... 68% 86.1M 4s
180900K .......... .......... .......... .......... .......... 68% 90.5M 4s
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181000K .......... .......... .......... .......... .......... 68% 14.4M 4s
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181100K .......... .......... .......... .......... .......... 68% 9.30M 4s
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181300K .......... .......... .......... .......... .......... 68% 86.7M 4s
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181400K .......... .......... .......... .......... .......... 68% 91.1M 4s
181450K .......... .......... .......... .......... .......... 68% 65.2M 4s
181500K .......... .......... .......... .......... .......... 68%  109M 4s
181550K .......... .......... .......... .......... .......... 68% 66.6M 4s
181600K .......... .......... .......... .......... .......... 68% 65.1M 4s
181650K .......... .......... .......... .......... .......... 68%  139M 4s
181700K .......... .......... .......... .......... .......... 68% 91.8M 4s
181750K .......... .......... .......... .......... .......... 68%  116M 4s
181800K .......... .......... .......... .......... .......... 68%  102M 4s
181850K .......... .......... .......... .......... .......... 68%  134M 4s
181900K .......... .......... .......... .......... .......... 68%  156M 4s
181950K .......... .......... .......... .......... .......... 68% 79.9M 4s
182000K .......... .......... .......... .......... .......... 68%  137M 4s
182050K .......... .......... .......... .......... .......... 68%  121M 4s
182100K .......... .......... .......... .......... .......... 68%  107M 4s
182150K .......... .......... .......... .......... .......... 68% 61.6M 4s
182200K .......... .......... .......... .......... .......... 68% 28.8M 4s
182250K .......... .......... .......... .......... .......... 68% 58.0M 4s
182300K .......... .......... .......... .......... .......... 68% 97.0M 4s
182350K .......... .......... .......... .......... .......... 68% 47.2M 4s
182400K .......... .......... .......... .......... .......... 68% 44.2M 4s
182450K .......... .......... .......... .......... .......... 68% 33.3M 4s
182500K .......... .......... .......... .......... .......... 68% 50.2M 4s
182550K .......... .......... .......... .......... .......... 68% 80.4M 4s
182600K .......... .......... .......... .......... .......... 68% 52.0M 4s
182650K .......... .......... .......... .......... .......... 68% 27.9M 4s
182700K .......... .......... .......... .......... .......... 68% 50.7M 4s
182750K .......... .......... .......... .......... .......... 68% 55.4M 4s
182800K .......... .......... .......... .......... .......... 68% 90.6M 3s
182850K .......... .......... .......... .......... .......... 68% 31.1M 3s
182900K .......... .......... .......... .......... .......... 68% 44.7M 3s
182950K .......... .......... .......... .......... .......... 68% 50.5M 3s
183000K .......... .......... .......... .......... .......... 68%  119M 3s
183050K .......... .......... .......... .......... .......... 68% 52.0M 3s
183100K .......... .......... .......... .......... .......... 68% 31.7M 3s
183150K .......... .......... .......... .......... .......... 68% 39.5M 3s
183200K .......... .......... .......... .......... .......... 68% 84.8M 3s
183250K .......... .......... .......... .......... .......... 68% 64.7M 3s
183300K .......... .......... .......... .......... .......... 68% 36.6M 3s
183350K .......... .......... .......... .......... .......... 68% 19.7M 3s
183400K .......... .......... .......... .......... .......... 69%  167M 3s
183450K .......... .......... .......... .......... .......... 69%  151M 3s
183500K .......... .......... .......... .......... .......... 69%  225M 3s
183550K .......... .......... .......... .......... .......... 69% 11.7M 3s
183600K .......... .......... .......... .......... .......... 69% 16.4M 3s
183650K .......... .......... .......... .......... .......... 69%  114M 3s
183700K .......... .......... .......... .......... .......... 69% 97.0M 3s
183750K .......... .......... .......... .......... .......... 69%  137M 3s
183800K .......... .......... .......... .......... .......... 69% 80.0M 3s
183850K .......... .......... .......... .......... .......... 69%  102M 3s
183900K .......... .......... .......... .......... .......... 69%  126M 3s
183950K .......... .......... .......... .......... .......... 69% 97.2M 3s
184000K .......... .......... .......... .......... .......... 69% 83.0M 3s
184050K .......... .......... .......... .......... .......... 69% 49.3M 3s
184100K .......... .......... .......... .......... .......... 69% 41.7M 3s
184150K .......... .......... .......... .......... .......... 69% 34.3M 3s
184200K .......... .......... .......... .......... .......... 69% 75.7M 3s
184250K .......... .......... .......... .......... .......... 69% 49.2M 3s
184300K .......... .......... .......... .......... .......... 69% 55.2M 3s
184350K .......... .......... .......... .......... .......... 69% 28.2M 3s
184400K .......... .......... .......... .......... .......... 69% 52.4M 3s
184450K .......... .......... .......... .......... .......... 69%  110M 3s
184500K .......... .......... .......... .......... .......... 69% 47.3M 3s
184550K .......... .......... .......... .......... .......... 69% 29.7M 3s
184600K .......... .......... .......... .......... .......... 69% 50.1M 3s
184650K .......... .......... .......... .......... .......... 69% 19.3M 3s
184700K .......... .......... .......... .......... .......... 69% 41.7M 3s
184750K .......... .......... .......... .......... .......... 69% 27.9M 3s
184800K .......... .......... .......... .......... .......... 69% 34.8M 3s
184850K .......... .......... .......... .......... .......... 69% 69.1M 3s
184900K .......... .......... .......... .......... .......... 69%  140M 3s
184950K .......... .......... .......... .......... .......... 69% 19.0M 3s
185000K .......... .......... .......... .......... .......... 69%  140M 3s
185050K .......... .......... .......... .......... .......... 69%  172M 3s
185100K .......... .......... .......... .......... .......... 69% 84.1M 3s
185150K .......... .......... .......... .......... .......... 69%  195M 3s
185200K .......... .......... .......... .......... .......... 69%  128M 3s
185250K .......... .......... .......... .......... .......... 69%  186M 3s
185300K .......... .......... .......... .......... .......... 69%  225M 3s
185350K .......... .......... .......... .......... .......... 69% 59.9M 3s
185400K .......... .......... .......... .......... .......... 69% 86.0M 3s
185450K .......... .......... .......... .......... .......... 69% 34.5M 3s
185500K .......... .......... .......... .......... .......... 69% 54.6M 3s
185550K .......... .......... .......... .......... .......... 69% 50.4M 3s
185600K .......... .......... .......... .......... .......... 69% 81.1M 3s
185650K .......... .......... .......... .......... .......... 69% 71.0M 3s
185700K .......... .......... .......... .......... .......... 69% 35.9M 3s
185750K .......... .......... .......... .......... .......... 69% 57.9M 3s
185800K .......... .......... .......... .......... .......... 69% 49.9M 3s
185850K .......... .......... .......... .......... .......... 69% 90.3M 3s
185900K .......... .......... .......... .......... .......... 69% 57.0M 3s
185950K .......... .......... .......... .......... .......... 69% 44.1M 3s
186000K .......... .......... .......... .......... .......... 69% 52.6M 3s
186050K .......... .......... .......... .......... .......... 70% 94.0M 3s
186100K .......... .......... .......... .......... .......... 70% 48.0M 3s
186150K .......... .......... .......... .......... .......... 70% 48.2M 3s
186200K .......... .......... .......... .......... .......... 70% 45.5M 3s
186250K .......... .......... .......... .......... .......... 70% 59.0M 3s
186300K .......... .......... .......... .......... .......... 70%  109M 3s
186350K .......... .......... .......... .......... .......... 70% 45.1M 3s
186400K .......... .......... .......... .......... .......... 70% 49.5M 3s
186450K .......... .......... .......... .......... .......... 70% 10.2M 3s
186500K .......... .......... .......... .......... .......... 70% 99.5M 3s
186550K .......... .......... .......... .......... .......... 70%  129M 3s
186600K .......... .......... .......... .......... .......... 70% 86.3M 3s
186650K .......... .......... .......... .......... .......... 70%  144M 3s
186700K .......... .......... .......... .......... .......... 70%  103M 3s
186750K .......... .......... .......... .......... .......... 70%  118M 3s
186800K .......... .......... .......... .......... .......... 70% 64.1M 3s
186850K .......... .......... .......... .......... .......... 70% 57.9M 3s
186900K .......... .......... .......... .......... .......... 70%  109M 3s
186950K .......... .......... .......... .......... .......... 70% 71.7M 3s
187000K .......... .......... .......... .......... .......... 70%  115M 3s
187050K .......... .......... .......... .......... .......... 70% 15.7M 3s
187100K .......... .......... .......... .......... .......... 70% 90.4M 3s
187150K .......... .......... .......... .......... .......... 70%  108M 3s
187200K .......... .......... .......... .......... .......... 70% 71.5M 3s
187250K .......... .......... .......... .......... .......... 70%  143M 3s
187300K .......... .......... .......... .......... .......... 70% 14.8M 3s
187350K .......... .......... .......... .......... .......... 70%  134M 3s
187400K .......... .......... .......... .......... .......... 70% 87.8M 3s
187450K .......... .......... .......... .......... .......... 70%  111M 3s
187500K .......... .......... .......... .......... .......... 70%  126M 3s
187550K .......... .......... .......... .......... .......... 70% 43.3M 3s
187600K .......... .......... .......... .......... .......... 70% 61.6M 3s
187650K .......... .......... .......... .......... .......... 70% 77.3M 3s
187700K .......... .......... .......... .......... .......... 70% 38.6M 3s
187750K .......... .......... .......... .......... .......... 70%  104M 3s
187800K .......... .......... .......... .......... .......... 70% 44.4M 3s
187850K .......... .......... .......... .......... .......... 70% 57.8M 3s
187900K .......... .......... .......... .......... .......... 70%  105M 3s
187950K .......... .......... .......... .......... .......... 70% 54.1M 3s
188000K .......... .......... .......... .......... .......... 70% 88.5M 3s
188050K .......... .......... .......... .......... .......... 70% 30.3M 3s
188100K .......... .......... .......... .......... .......... 70% 47.8M 3s
188150K .......... .......... .......... .......... .......... 70%  135M 3s
188200K .......... .......... .......... .......... .......... 70% 16.6M 3s
188250K .......... .......... .......... .......... .......... 70% 93.0M 3s
188300K .......... .......... .......... .......... .......... 70% 91.8M 3s
188350K .......... .......... .......... .......... .......... 70%  108M 3s
188400K .......... .......... .......... .......... .......... 70% 11.6M 3s
188450K .......... .......... .......... .......... .......... 70%  125M 3s
188500K .......... .......... .......... .......... .......... 70%  112M 3s
188550K .......... .......... .......... .......... .......... 70%  115M 3s
188600K .......... .......... .......... .......... .......... 70%  133M 3s
188650K .......... .......... .......... .......... .......... 70%  199M 3s
188700K .......... .......... .......... .......... .......... 71%  188M 3s
188750K .......... .......... .......... .......... .......... 71% 10.0M 3s
188800K .......... .......... .......... .......... .......... 71%  107M 3s
188850K .......... .......... .......... .......... .......... 71%  124M 3s
188900K .......... .......... .......... .......... .......... 71% 97.6M 3s
188950K .......... .......... .......... .......... .......... 71%  130M 3s
189000K .......... .......... .......... .......... .......... 71%  174M 3s
189050K .......... .......... .......... .......... .......... 71% 24.5M 3s
189100K .......... .......... .......... .......... .......... 71% 89.8M 3s
189150K .......... .......... .......... .......... .......... 71%  101M 3s
189200K .......... .......... .......... .......... .......... 71% 62.3M 3s
189250K .......... .......... .......... .......... .......... 71% 75.9M 3s
189300K .......... .......... .......... .......... .......... 71% 19.9M 3s
189350K .......... .......... .......... .......... .......... 71% 39.1M 3s
189400K .......... .......... .......... .......... .......... 71% 41.4M 3s
189450K .......... .......... .......... .......... .......... 71% 68.6M 3s
189500K .......... .......... .......... .......... .......... 71% 99.5M 3s
189550K .......... .......... .......... .......... .......... 71% 9.25M 3s
189600K .......... .......... .......... .......... .......... 71% 29.6M 3s
189650K .......... .......... .......... .......... .......... 71% 24.2M 3s
189700K .......... .......... .......... .......... .......... 71% 24.3M 3s
189750K .......... .......... .......... .......... .......... 71%  140M 3s
189800K .......... .......... .......... .......... .......... 71% 27.1M 3s
189850K .......... .......... .......... .......... .......... 71% 25.1M 3s
189900K .......... .......... .......... .......... .......... 71% 76.3M 3s
189950K .......... .......... .......... .......... .......... 71%  142M 3s
190000K .......... .......... .......... .......... .......... 71%  180M 3s
190050K .......... .......... .......... .......... .......... 71% 70.8M 3s
190100K .......... .......... .......... .......... .......... 71% 40.1M 3s
190150K .......... .......... .......... .......... .......... 71% 24.1M 3s
190200K .......... .......... .......... .......... .......... 71% 18.8M 3s
190250K .......... .......... .......... .......... .......... 71%  154M 3s
190300K .......... .......... .......... .......... .......... 71% 74.0M 3s
190350K .......... .......... .......... .......... .......... 71% 33.8M 3s
190400K .......... .......... .......... .......... .......... 71% 20.6M 3s
190450K .......... .......... .......... .......... .......... 71%  124M 3s
190500K .......... .......... .......... .......... .......... 71% 39.7M 3s
190550K .......... .......... .......... .......... .......... 71% 49.3M 3s
190600K .......... .......... .......... .......... .......... 71% 51.5M 3s
190650K .......... .......... .......... .......... .......... 71% 64.7M 3s
190700K .......... .......... .......... .......... .......... 71% 43.1M 3s
190750K .......... .......... .......... .......... .......... 71% 60.5M 3s
190800K .......... .......... .......... .......... .......... 71% 31.6M 3s
190850K .......... .......... .......... .......... .......... 71% 22.3M 3s
190900K .......... .......... .......... .......... .......... 71% 47.4M 3s
190950K .......... .......... .......... .......... .......... 71% 75.4M 3s
191000K .......... .......... .......... .......... .......... 71%  105M 3s
191050K .......... .......... .......... .......... .......... 71% 92.3M 3s
191100K .......... .......... .......... .......... .......... 71% 61.6M 3s
191150K .......... .......... .......... .......... .......... 71% 38.3M 3s
191200K .......... .......... .......... .......... .......... 71% 56.0M 3s
191250K .......... .......... .......... .......... .......... 71% 63.3M 3s
191300K .......... .......... .......... .......... .......... 71%  254M 3s
191350K .......... .......... .......... .......... .......... 72% 60.9M 3s
191400K .......... .......... .......... .......... .......... 72% 38.6M 3s
191450K .......... .......... .......... .......... .......... 72% 32.5M 3s
191500K .......... .......... .......... .......... .......... 72% 95.5M 3s
191550K .......... .......... .......... .......... .......... 72%  112M 3s
191600K .......... .......... .......... .......... .......... 72% 71.9M 3s
191650K .......... .......... .......... .......... .......... 72%  201M 3s
191700K .......... .......... .......... .......... .......... 72% 88.7M 3s
191750K .......... .......... .......... .......... .......... 72% 71.5M 3s
191800K .......... .......... .......... .......... .......... 72% 78.3M 3s
191850K .......... .......... .......... .......... .......... 72% 32.4M 3s
191900K .......... .......... .......... .......... .......... 72% 43.8M 3s
191950K .......... .......... .......... .......... .......... 72% 80.2M 3s
192000K .......... .......... .......... .......... .......... 72%  152M 3s
192050K .......... .......... .......... .......... .......... 72% 90.9M 3s
192100K .......... .......... .......... .......... .......... 72% 53.5M 3s
192150K .......... .......... .......... .......... .......... 72%  108M 3s
192200K .......... .......... .......... .......... .......... 72% 63.3M 3s
192250K .......... .......... .......... .......... .......... 72%  111M 3s
192300K .......... .......... .......... .......... .......... 72% 84.4M 3s
192350K .......... .......... .......... .......... .......... 72% 66.1M 3s
192400K .......... .......... .......... .......... .......... 72%  122M 3s
192450K .......... .......... .......... .......... .......... 72% 20.5M 3s
192500K .......... .......... .......... .......... .......... 72% 49.6M 3s
192550K .......... .......... .......... .......... .......... 72% 28.5M 3s
192600K .......... .......... .......... .......... .......... 72% 46.1M 3s
192650K .......... .......... .......... .......... .......... 72% 83.4M 3s
192700K .......... .......... .......... .......... .......... 72% 22.8M 3s
192750K .......... .......... .......... .......... .......... 72% 62.3M 3s
192800K .......... .......... .......... .......... .......... 72% 62.3M 3s
192850K .......... .......... .......... .......... .......... 72% 46.5M 3s
192900K .......... .......... .......... .......... .......... 72% 42.0M 3s
192950K .......... .......... .......... .......... .......... 72% 29.7M 3s
193000K .......... .......... .......... .......... .......... 72%  122M 3s
193050K .......... .......... .......... .......... .......... 72%  168M 3s
193100K .......... .......... .......... .......... .......... 72%  204M 3s
193150K .......... .......... .......... .......... .......... 72% 24.1M 3s
193200K .......... .......... .......... .......... .......... 72% 23.3M 3s
193250K .......... .......... .......... .......... .......... 72%  126M 3s
193300K .......... .......... .......... .......... .......... 72%  170M 3s
193350K .......... .......... .......... .......... .......... 72%  156M 3s
193400K .......... .......... .......... .......... .......... 72%  144M 3s
193450K .......... .......... .......... .......... .......... 72%  139M 3s
193500K .......... .......... .......... .......... .......... 72% 42.4M 3s
193550K .......... .......... .......... .......... .......... 72% 28.3M 3s
193600K .......... .......... .......... .......... .......... 72% 35.0M 3s
193650K .......... .......... .......... .......... .......... 72% 21.3M 3s
193700K .......... .......... .......... .......... .......... 72% 17.6M 3s
193750K .......... .......... .......... .......... .......... 72% 27.7M 3s
193800K .......... .......... .......... .......... .......... 72% 12.5M 3s
193850K .......... .......... .......... .......... .......... 72% 21.6M 3s
193900K .......... .......... .......... .......... .......... 72% 23.1M 3s
193950K .......... .......... .......... .......... .......... 72% 43.9M 3s
194000K .......... .......... .......... .......... .......... 73% 32.5M 3s
194050K .......... .......... .......... .......... .......... 73% 35.5M 3s
194100K .......... .......... .......... .......... .......... 73% 34.5M 3s
194150K .......... .......... .......... .......... .......... 73% 61.3M 3s
194200K .......... .......... .......... .......... .......... 73% 33.7M 3s
194250K .......... .......... .......... .......... .......... 73% 80.5M 3s
194300K .......... .......... .......... .......... .......... 73% 63.6M 3s
194350K .......... .......... .......... .......... .......... 73% 36.9M 3s
194400K .......... .......... .......... .......... .......... 73%  168M 3s
194450K .......... .......... .......... .......... .......... 73% 67.0M 3s
194500K .......... .......... .......... .......... .......... 73% 97.9M 3s
194550K .......... .......... .......... .......... .......... 73% 46.7M 3s
194600K .......... .......... .......... .......... .......... 73%  103M 3s
194650K .......... .......... .......... .......... .......... 73%  167M 3s
194700K .......... .......... .......... .......... .......... 73%  139M 3s
194750K .......... .......... .......... .......... .......... 73%  161M 3s
194800K .......... .......... .......... .......... .......... 73% 56.9M 3s
194850K .......... .......... .......... .......... .......... 73% 40.7M 3s
194900K .......... .......... .......... .......... .......... 73% 86.3M 3s
194950K .......... .......... .......... .......... .......... 73%  129M 3s
195000K .......... .......... .......... .......... .......... 73% 62.5M 3s
195050K .......... .......... .......... .......... .......... 73% 35.7M 3s
195100K .......... .......... .......... .......... .......... 73% 37.5M 3s
195150K .......... .......... .......... .......... .......... 73% 33.1M 3s
195200K .......... .......... .......... .......... .......... 73% 19.9M 3s
195250K .......... .......... .......... .......... .......... 73% 57.6M 3s
195300K .......... .......... .......... .......... .......... 73% 78.2M 3s
195350K .......... .......... .......... .......... .......... 73% 42.7M 3s
195400K .......... .......... .......... .......... .......... 73% 81.0M 3s
195450K .......... .......... .......... .......... .......... 73% 65.8M 3s
195500K .......... .......... .......... .......... .......... 73% 73.6M 3s
195550K .......... .......... .......... .......... .......... 73% 65.8M 3s
195600K .......... .......... .......... .......... .......... 73% 75.1M 3s
195650K .......... .......... .......... .......... .......... 73%  118M 3s
195700K .......... .......... .......... .......... .......... 73% 67.6M 3s
195750K .......... .......... .......... .......... .......... 73% 63.9M 3s
195800K .......... .......... .......... .......... .......... 73%  116M 3s
195850K .......... .......... .......... .......... .......... 73% 55.6M 3s
195900K .......... .......... .......... .......... .......... 73% 48.3M 3s
195950K .......... .......... .......... .......... .......... 73% 20.4M 3s
196000K .......... .......... .......... .......... .......... 73% 24.6M 3s
196050K .......... .......... .......... .......... .......... 73% 50.7M 3s
196100K .......... .......... .......... .......... .......... 73% 38.3M 3s
196150K .......... .......... .......... .......... .......... 73% 34.2M 3s
196200K .......... .......... .......... .......... .......... 73% 51.2M 3s
196250K .......... .......... .......... .......... .......... 73% 72.8M 3s
196300K .......... .......... .......... .......... .......... 73% 26.2M 3s
196350K .......... .......... .......... .......... .......... 73% 33.5M 3s
196400K .......... .......... .......... .......... .......... 73% 69.0M 3s
196450K .......... .......... .......... .......... .......... 73% 46.3M 3s
196500K .......... .......... .......... .......... .......... 73% 39.7M 3s
196550K .......... .......... .......... .......... .......... 73% 47.8M 3s
196600K .......... .......... .......... .......... .......... 73% 19.6M 3s
196650K .......... .......... .......... .......... .......... 74% 16.6M 3s
196700K .......... .......... .......... .......... .......... 74% 17.8M 3s
196750K .......... .......... .......... .......... .......... 74% 79.6M 3s
196800K .......... .......... .......... .......... .......... 74% 63.5M 3s
196850K .......... .......... .......... .......... .......... 74% 68.8M 3s
196900K .......... .......... .......... .......... .......... 74% 16.4M 3s
196950K .......... .......... .......... .......... .......... 74% 78.7M 3s
197000K .......... .......... .......... .......... .......... 74% 66.7M 3s
197050K .......... .......... .......... .......... .......... 74% 74.0M 3s
197100K .......... .......... .......... .......... .......... 74% 68.5M 3s
197150K .......... .......... .......... .......... .......... 74% 87.2M 3s
197200K .......... .......... .......... .......... .......... 74% 53.1M 3s
197250K .......... .......... .......... .......... .......... 74%  150M 3s
197300K .......... .......... .......... .......... .......... 74% 92.9M 3s
197350K .......... .......... .......... .......... .......... 74%  126M 3s
197400K .......... .......... .......... .......... .......... 74% 66.2M 3s
197450K .......... .......... .......... .......... .......... 74% 50.4M 3s
197500K .......... .......... .......... .......... .......... 74% 59.8M 3s
197550K .......... .......... .......... .......... .......... 74% 31.6M 3s
197600K .......... .......... .......... .......... .......... 74% 59.3M 3s
197650K .......... .......... .......... .......... .......... 74% 75.7M 3s
197700K .......... .......... .......... .......... .......... 74% 57.5M 3s
197750K .......... .......... .......... .......... .......... 74% 63.1M 3s
197800K .......... .......... .......... .......... .......... 74% 46.2M 3s
197850K .......... .......... .......... .......... .......... 74% 16.1M 3s
197900K .......... .......... .......... .......... .......... 74% 13.0M 3s
197950K .......... .......... .......... .......... .......... 74% 35.8M 3s
198000K .......... .......... .......... .......... .......... 74% 57.1M 3s
198050K .......... .......... .......... .......... .......... 74% 33.8M 3s
198100K .......... .......... .......... .......... .......... 74% 38.8M 3s
198150K .......... .......... .......... .......... .......... 74% 50.7M 3s
198200K .......... .......... .......... .......... .......... 74% 65.2M 3s
198250K .......... .......... .......... .......... .......... 74% 71.8M 3s
198300K .......... .......... .......... .......... .......... 74% 64.0M 3s
198350K .......... .......... .......... .......... .......... 74% 53.7M 3s
198400K .......... .......... .......... .......... .......... 74% 97.1M 3s
198450K .......... .......... .......... .......... .......... 74% 52.2M 3s
198500K .......... .......... .......... .......... .......... 74% 88.3M 3s
198550K .......... .......... .......... .......... .......... 74% 61.2M 3s
198600K .......... .......... .......... .......... .......... 74% 20.4M 3s
198650K .......... .......... .......... .......... .......... 74% 71.1M 3s
198700K .......... .......... .......... .......... .......... 74% 79.7M 3s
198750K .......... .......... .......... .......... .......... 74% 39.4M 3s
198800K .......... .......... .......... .......... .......... 74%  106M 3s
198850K .......... .......... .......... .......... .......... 74% 59.0M 3s
198900K .......... .......... .......... .......... .......... 74% 83.2M 3s
198950K .......... .......... .......... .......... .......... 74% 56.6M 3s
199000K .......... .......... .......... .......... .......... 74% 68.5M 3s
199050K .......... .......... .......... .......... .......... 74% 40.1M 3s
199100K .......... .......... .......... .......... .......... 74% 69.6M 3s
199150K .......... .......... .......... .......... .......... 74% 65.7M 3s
199200K .......... .......... .......... .......... .......... 74% 73.3M 3s
199250K .......... .......... .......... .......... .......... 74% 48.8M 3s
199300K .......... .......... .......... .......... .......... 74%  113M 3s
199350K .......... .......... .......... .......... .......... 75%  139M 3s
199400K .......... .......... .......... .......... .......... 75% 32.8M 3s
199450K .......... .......... .......... .......... .......... 75% 44.9M 3s
199500K .......... .......... .......... .......... .......... 75% 38.7M 3s
199550K .......... .......... .......... .......... .......... 75%  158M 3s
199600K .......... .......... .......... .......... .......... 75%  140M 3s
199650K .......... .......... .......... .......... .......... 75%  151M 3s
199700K .......... .......... .......... .......... .......... 75%  151M 3s
199750K .......... .......... .......... .......... .......... 75%  108M 3s
199800K .......... .......... .......... .......... .......... 75%  114M 3s
199850K .......... .......... .......... .......... .......... 75% 96.8M 3s
199900K .......... .......... .......... .......... .......... 75%  145M 3s
199950K .......... .......... .......... .......... .......... 75%  131M 3s
200000K .......... .......... .......... .......... .......... 75%  165M 3s
200050K .......... .......... .......... .......... .......... 75%  128M 3s
200100K .......... .......... .......... .......... .......... 75%  177M 3s
200150K .......... .......... .......... .......... .......... 75%  191M 3s
200200K .......... .......... .......... .......... .......... 75%  145M 3s
200250K .......... .......... .......... .......... .......... 75%  170M 3s
200300K .......... .......... .......... .......... .......... 75%  133M 3s
200350K .......... .......... .......... .......... .......... 75%  144M 3s
200400K .......... .......... .......... .......... .......... 75%  142M 3s
200450K .......... .......... .......... .......... .......... 75%  146M 3s
200500K .......... .......... .......... .......... .......... 75%  193M 3s
200550K .......... .......... .......... .......... .......... 75%  150M 3s
200600K .......... .......... .......... .......... .......... 75%  137M 3s
200650K .......... .......... .......... .......... .......... 75%  125M 3s
200700K .......... .......... .......... .......... .......... 75%  179M 3s
200750K .......... .......... .......... .......... .......... 75%  169M 3s
200800K .......... .......... .......... .......... .......... 75%  165M 3s
200850K .......... .......... .......... .......... .......... 75%  168M 3s
200900K .......... .......... .......... .......... .......... 75%  176M 3s
200950K .......... .......... .......... .......... .......... 75%  124M 3s
201000K .......... .......... .......... .......... .......... 75% 98.9M 3s
201050K .......... .......... .......... .......... .......... 75%  167M 3s
201100K .......... .......... .......... .......... .......... 75%  177M 3s
201150K .......... .......... .......... .......... .......... 75%  222M 3s
201200K .......... .......... .......... .......... .......... 75%  251M 3s
201250K .......... .......... .......... .......... .......... 75%  176M 3s
201300K .......... .......... .......... .......... .......... 75% 78.7M 3s
201350K .......... .......... .......... .......... .......... 75%  127M 3s
201400K .......... .......... .......... .......... .......... 75%  199M 3s
201450K .......... .......... .......... .......... .......... 75%  131M 3s
201500K .......... .......... .......... .......... .......... 75%  168M 3s
201550K .......... .......... .......... .......... .......... 75%  151M 3s
201600K .......... .......... .......... .......... .......... 75%  129M 3s
201650K .......... .......... .......... .......... .......... 75%  216M 3s
201700K .......... .......... .......... .......... .......... 75%  103M 3s
201750K .......... .......... .......... .......... .......... 75%  255M 3s
201800K .......... .......... .......... .......... .......... 75%  252M 3s
201850K .......... .......... .......... .......... .......... 75%  158M 3s
201900K .......... .......... .......... .......... .......... 75%  131M 3s
201950K .......... .......... .......... .......... .......... 75%  207M 3s
202000K .......... .......... .......... .......... .......... 76%  208M 3s
202050K .......... .......... .......... .......... .......... 76% 43.3M 3s
202100K .......... .......... .......... .......... .......... 76% 53.8M 3s
202150K .......... .......... .......... .......... .......... 76% 43.1M 3s
202200K .......... .......... .......... .......... .......... 76% 92.9M 3s
202250K .......... .......... .......... .......... .......... 76% 32.4M 3s
202300K .......... .......... .......... .......... .......... 76% 91.1M 3s
202350K .......... .......... .......... .......... .......... 76% 34.2M 3s
202400K .......... .......... .......... .......... .......... 76% 60.4M 3s
202450K .......... .......... .......... .......... .......... 76% 13.3M 3s
202500K .......... .......... .......... .......... .......... 76%  118M 3s
202550K .......... .......... .......... .......... .......... 76%  175M 3s
202600K .......... .......... .......... .......... .......... 76%  169M 3s
202650K .......... .......... .......... .......... .......... 76% 14.1M 3s
202700K .......... .......... .......... .......... .......... 76% 18.8M 3s
202750K .......... .......... .......... .......... .......... 76% 25.2M 3s
202800K .......... .......... .......... .......... .......... 76% 27.7M 3s
202850K .......... .......... .......... .......... .......... 76%  162M 3s
202900K .......... .......... .......... .......... .......... 76%  109M 3s
202950K .......... .......... .......... .......... .......... 76% 52.1M 3s
203000K .......... .......... .......... .......... .......... 76% 52.7M 3s
203050K .......... .......... .......... .......... .......... 76% 41.3M 3s
203100K .......... .......... .......... .......... .......... 76% 31.2M 2s
203150K .......... .......... .......... .......... .......... 76% 51.9M 2s
203200K .......... .......... .......... .......... .......... 76% 26.3M 2s
203250K .......... .......... .......... .......... .......... 76% 36.3M 2s
203300K .......... .......... .......... .......... .......... 76% 67.4M 2s
203350K .......... .......... .......... .......... .......... 76% 68.7M 2s
203400K .......... .......... .......... .......... .......... 76% 19.0M 2s
203450K .......... .......... .......... .......... .......... 76% 20.4M 2s
203500K .......... .......... .......... .......... .......... 76% 91.3M 2s
203550K .......... .......... .......... .......... .......... 76%  139M 2s
203600K .......... .......... .......... .......... .......... 76% 90.4M 2s
203650K .......... .......... .......... .......... .......... 76% 61.5M 2s
203700K .......... .......... .......... .......... .......... 76% 74.8M 2s
203750K .......... .......... .......... .......... .......... 76% 10.2M 2s
203800K .......... .......... .......... .......... .......... 76% 70.9M 2s
203850K .......... .......... .......... .......... .......... 76% 68.6M 2s
203900K .......... .......... .......... .......... .......... 76% 50.2M 2s
203950K .......... .......... .......... .......... .......... 76% 53.9M 2s
204000K .......... .......... .......... .......... .......... 76% 76.0M 2s
204050K .......... .......... .......... .......... .......... 76% 86.0M 2s
204100K .......... .......... .......... .......... .......... 76% 57.9M 2s
204150K .......... .......... .......... .......... .......... 76% 79.5M 2s
204200K .......... .......... .......... .......... .......... 76% 92.4M 2s
204250K .......... .......... .......... .......... .......... 76% 66.3M 2s
204300K .......... .......... .......... .......... .......... 76% 67.2M 2s
204350K .......... .......... .......... .......... .......... 76% 54.9M 2s
204400K .......... .......... .......... .......... .......... 76% 49.6M 2s
204450K .......... .......... .......... .......... .......... 76% 50.5M 2s
204500K .......... .......... .......... .......... .......... 76% 96.2M 2s
204550K .......... .......... .......... .......... .......... 76% 99.9M 2s
204600K .......... .......... .......... .......... .......... 76% 79.0M 2s
204650K .......... .......... .......... .......... .......... 77% 76.8M 2s
204700K .......... .......... .......... .......... .......... 77%  191M 2s
204750K .......... .......... .......... .......... .......... 77%  250M 2s
204800K .......... .......... .......... .......... .......... 77% 64.4M 2s
204850K .......... .......... .......... .......... .......... 77%  169M 2s
204900K .......... .......... .......... .......... .......... 77%  119M 2s
204950K .......... .......... .......... .......... .......... 77% 32.3M 2s
205000K .......... .......... .......... .......... .......... 77%  145M 2s
205050K .......... .......... .......... .......... .......... 77%  163M 2s
205100K .......... .......... .......... .......... .......... 77%  164M 2s
205150K .......... .......... .......... .......... .......... 77%  230M 2s
205200K .......... .......... .......... .......... .......... 77%  158M 2s
205250K .......... .......... .......... .......... .......... 77%  201M 2s
205300K .......... .......... .......... .......... .......... 77%  257M 2s
205350K .......... .......... .......... .......... .......... 77%  168M 2s
205400K .......... .......... .......... .......... .......... 77% 17.1M 2s
205450K .......... .......... .......... .......... .......... 77%  103M 2s
205500K .......... .......... .......... .......... .......... 77% 63.7M 2s
205550K .......... .......... .......... .......... .......... 77% 81.7M 2s
205600K .......... .......... .......... .......... .......... 77% 64.9M 2s
205650K .......... .......... .......... .......... .......... 77% 44.9M 2s
205700K .......... .......... .......... .......... .......... 77% 66.0M 2s
205750K .......... .......... .......... .......... .......... 77% 47.1M 2s
205800K .......... .......... .......... .......... .......... 77% 53.3M 2s
205850K .......... .......... .......... .......... .......... 77% 33.0M 2s
205900K .......... .......... .......... .......... .......... 77% 60.8M 2s
205950K .......... .......... .......... .......... .......... 77% 36.4M 2s
206000K .......... .......... .......... .......... .......... 77%  101M 2s
206050K .......... .......... .......... .......... .......... 77% 36.5M 2s
206100K .......... .......... .......... .......... .......... 77% 25.9M 2s
206150K .......... .......... .......... .......... .......... 77% 24.6M 2s
206200K .......... .......... .......... .......... .......... 77% 22.3M 2s
206250K .......... .......... .......... .......... .......... 77% 34.2M 2s
206300K .......... .......... .......... .......... .......... 77% 11.9M 2s
206350K .......... .......... .......... .......... .......... 77% 63.2M 2s
206400K .......... .......... .......... .......... .......... 77% 89.1M 2s
206450K .......... .......... .......... .......... .......... 77%  134M 2s
206500K .......... .......... .......... .......... .......... 77% 94.0M 2s
206550K .......... .......... .......... .......... .......... 77% 75.0M 2s
206600K .......... .......... .......... .......... .......... 77% 96.0M 2s
206650K .......... .......... .......... .......... .......... 77%  106M 2s
206700K .......... .......... .......... .......... .......... 77% 97.5M 2s
206750K .......... .......... .......... .......... .......... 77% 76.2M 2s
206800K .......... .......... .......... .......... .......... 77% 93.2M 2s
206850K .......... .......... .......... .......... .......... 77%  106M 2s
206900K .......... .......... .......... .......... .......... 77%  122M 2s
206950K .......... .......... .......... .......... .......... 77% 64.5M 2s
207000K .......... .......... .......... .......... .......... 77% 73.5M 2s
207050K .......... .......... .......... .......... .......... 77%  126M 2s
207100K .......... .......... .......... .......... .......... 77%  132M 2s
207150K .......... .......... .......... .......... .......... 77%  142M 2s
207200K .......... .......... .......... .......... .......... 77%  104M 2s
207250K .......... .......... .......... .......... .......... 77% 95.3M 2s
207300K .......... .......... .......... .......... .......... 78%  105M 2s
207350K .......... .......... .......... .......... .......... 78% 99.7M 2s
207400K .......... .......... .......... .......... .......... 78% 9.42M 2s
207450K .......... .......... .......... .......... .......... 78%  129M 2s
207500K .......... .......... .......... .......... .......... 78%  112M 2s
207550K .......... .......... .......... .......... .......... 78% 95.1M 2s
207600K .......... .......... .......... .......... .......... 78% 68.4M 2s
207650K .......... .......... .......... .......... .......... 78% 94.3M 2s
207700K .......... .......... .......... .......... .......... 78% 21.2M 2s
207750K .......... .......... .......... .......... .......... 78% 51.4M 2s
207800K .......... .......... .......... .......... .......... 78% 46.0M 2s
207850K .......... .......... .......... .......... .......... 78% 31.1M 2s
207900K .......... .......... .......... .......... .......... 78% 65.1M 2s
207950K .......... .......... .......... .......... .......... 78% 70.2M 2s
208000K .......... .......... .......... .......... .......... 78% 37.4M 2s
208050K .......... .......... .......... .......... .......... 78% 35.1M 2s
208100K .......... .......... .......... .......... .......... 78% 41.9M 2s
208150K .......... .......... .......... .......... .......... 78% 92.8M 2s
208200K .......... .......... .......... .......... .......... 78% 37.5M 2s
208250K .......... .......... .......... .......... .......... 78% 46.0M 2s
208300K .......... .......... .......... .......... .......... 78% 46.7M 2s
208350K .......... .......... .......... .......... .......... 78% 25.9M 2s
208400K .......... .......... .......... .......... .......... 78% 17.7M 2s
208450K .......... .......... .......... .......... .......... 78% 87.0M 2s
208500K .......... .......... .......... .......... .......... 78%  151M 2s
208550K .......... .......... .......... .......... .......... 78% 79.9M 2s
208600K .......... .......... .......... .......... .......... 78% 96.1M 2s
208650K .......... .......... .......... .......... .......... 78%  134M 2s
208700K .......... .......... .......... .......... .......... 78% 62.4M 2s
208750K .......... .......... .......... .......... .......... 78%  127M 2s
208800K .......... .......... .......... .......... .......... 78% 70.5M 2s
208850K .......... .......... .......... .......... .......... 78% 83.0M 2s
208900K .......... .......... .......... .......... .......... 78% 81.9M 2s
208950K .......... .......... .......... .......... .......... 78% 48.3M 2s
209000K .......... .......... .......... .......... .......... 78% 77.5M 2s
209050K .......... .......... .......... .......... .......... 78% 83.8M 2s
209100K .......... .......... .......... .......... .......... 78% 53.3M 2s
209150K .......... .......... .......... .......... .......... 78%  134M 2s
209200K .......... .......... .......... .......... .......... 78% 69.1M 2s
209250K .......... .......... .......... .......... .......... 78%  119M 2s
209300K .......... .......... .......... .......... .......... 78%  131M 2s
209350K .......... .......... .......... .......... .......... 78% 48.5M 2s
209400K .......... .......... .......... .......... .......... 78% 88.4M 2s
209450K .......... .......... .......... .......... .......... 78% 99.4M 2s
209500K .......... .......... .......... .......... .......... 78% 83.9M 2s
209550K .......... .......... .......... .......... .......... 78%  145M 2s
209600K .......... .......... .......... .......... .......... 78% 69.8M 2s
209650K .......... .......... .......... .......... .......... 78%  126M 2s
209700K .......... .......... .......... .......... .......... 78% 62.1M 2s
209750K .......... .......... .......... .......... .......... 78% 58.1M 2s
209800K .......... .......... .......... .......... .......... 78% 32.3M 2s
209850K .......... .......... .......... .......... .......... 78% 77.6M 2s
209900K .......... .......... .......... .......... .......... 78%  103M 2s
209950K .......... .......... .......... .......... .......... 79% 35.2M 2s
210000K .......... .......... .......... .......... .......... 79% 81.0M 2s
210050K .......... .......... .......... .......... .......... 79% 44.4M 2s
210100K .......... .......... .......... .......... .......... 79% 53.9M 2s
210150K .......... .......... .......... .......... .......... 79% 73.0M 2s
210200K .......... .......... .......... .......... .......... 79% 47.1M 2s
210250K .......... .......... .......... .......... .......... 79% 51.6M 2s
210300K .......... .......... .......... .......... .......... 79% 50.1M 2s
210350K .......... .......... .......... .......... .......... 79% 71.8M 2s
210400K .......... .......... .......... .......... .......... 79% 53.3M 2s
210450K .......... .......... .......... .......... .......... 79% 70.7M 2s
210500K .......... .......... .......... .......... .......... 79% 40.8M 2s
210550K .......... .......... .......... .......... .......... 79% 66.1M 2s
210600K .......... .......... .......... .......... .......... 79% 51.5M 2s
210650K .......... .......... .......... .......... .......... 79% 64.7M 2s
210700K .......... .......... .......... .......... .......... 79% 40.6M 2s
210750K .......... .......... .......... .......... .......... 79% 50.9M 2s
210800K .......... .......... .......... .......... .......... 79% 62.5M 2s
210850K .......... .......... .......... .......... .......... 79% 88.4M 2s
210900K .......... .......... .......... .......... .......... 79% 52.4M 2s
210950K .......... .......... .......... .......... .......... 79% 38.6M 2s
211000K .......... .......... .......... .......... .......... 79% 54.5M 2s
211050K .......... .......... .......... .......... .......... 79%  133M 2s
211100K .......... .......... .......... .......... .......... 79% 44.0M 2s
211150K .......... .......... .......... .......... .......... 79% 54.7M 2s
211200K .......... .......... .......... .......... .......... 79% 40.5M 2s
211250K .......... .......... .......... .......... .......... 79% 55.7M 2s
211300K .......... .......... .......... .......... .......... 79%  103M 2s
211350K .......... .......... .......... .......... .......... 79% 41.9M 2s
211400K .......... .......... .......... .......... .......... 79% 58.4M 2s
211450K .......... .......... .......... .......... .......... 79% 56.4M 2s
211500K .......... .......... .......... .......... .......... 79% 41.8M 2s
211550K .......... .......... .......... .......... .......... 79% 42.9M 2s
211600K .......... .......... .......... .......... .......... 79% 57.7M 2s
211650K .......... .......... .......... .......... .......... 79% 66.1M 2s
211700K .......... .......... .......... .......... .......... 79% 45.3M 2s
211750K .......... .......... .......... .......... .......... 79% 57.4M 2s
211800K .......... .......... .......... .......... .......... 79% 89.1M 2s
211850K .......... .......... .......... .......... .......... 79%  107M 2s
211900K .......... .......... .......... .......... .......... 79% 20.4M 2s
211950K .......... .......... .......... .......... .......... 79% 41.5M 2s
212000K .......... .......... .......... .......... .......... 79% 32.8M 2s
212050K .......... .......... .......... .......... .......... 79% 63.0M 2s
212100K .......... .......... .......... .......... .......... 79% 85.2M 2s
212150K .......... .......... .......... .......... .......... 79% 50.9M 2s
212200K .......... .......... .......... .......... .......... 79% 77.2M 2s
212250K .......... .......... .......... .......... .......... 79% 59.9M 2s
212300K .......... .......... .......... .......... .......... 79% 34.4M 2s
212350K .......... .......... .......... .......... .......... 79% 32.0M 2s
212400K .......... .......... .......... .......... .......... 79% 44.7M 2s
212450K .......... .......... .......... .......... .......... 79% 54.5M 2s
212500K .......... .......... .......... .......... .......... 79% 51.7M 2s
212550K .......... .......... .......... .......... .......... 79% 46.1M 2s
212600K .......... .......... .......... .......... .......... 80% 31.3M 2s
212650K .......... .......... .......... .......... .......... 80% 88.2M 2s
212700K .......... .......... .......... .......... .......... 80% 25.8M 2s
212750K .......... .......... .......... .......... .......... 80% 42.9M 2s
212800K .......... .......... .......... .......... .......... 80% 55.0M 2s
212850K .......... .......... .......... .......... .......... 80% 56.8M 2s
212900K .......... .......... .......... .......... .......... 80% 91.6M 2s
212950K .......... .......... .......... .......... .......... 80% 89.6M 2s
213000K .......... .......... .......... .......... .......... 80% 38.7M 2s
213050K .......... .......... .......... .......... .......... 80% 60.6M 2s
213100K .......... .......... .......... .......... .......... 80% 58.4M 2s
213150K .......... .......... .......... .......... .......... 80% 41.6M 2s
213200K .......... .......... .......... .......... .......... 80%  130M 2s
213250K .......... .......... .......... .......... .......... 80% 32.9M 2s
213300K .......... .......... .......... .......... .......... 80% 52.0M 2s
213350K .......... .......... .......... .......... .......... 80% 56.6M 2s
213400K .......... .......... .......... .......... .......... 80% 31.0M 2s
213450K .......... .......... .......... .......... .......... 80% 94.7M 2s
213500K .......... .......... .......... .......... .......... 80% 36.5M 2s
213550K .......... .......... .......... .......... .......... 80% 33.6M 2s
213600K .......... .......... .......... .......... .......... 80% 57.9M 2s
213650K .......... .......... .......... .......... .......... 80% 66.5M 2s
213700K .......... .......... .......... .......... .......... 80% 36.4M 2s
213750K .......... .......... .......... .......... .......... 80% 34.0M 2s
213800K .......... .......... .......... .......... .......... 80%  116M 2s
213850K .......... .......... .......... .......... .......... 80% 25.2M 2s
213900K .......... .......... .......... .......... .......... 80% 86.4M 2s
213950K .......... .......... .......... .......... .......... 80% 69.5M 2s
214000K .......... .......... .......... .......... .......... 80% 28.8M 2s
214050K .......... .......... .......... .......... .......... 80% 46.2M 2s
214100K .......... .......... .......... .......... .......... 80% 37.9M 2s
214150K .......... .......... .......... .......... .......... 80% 54.5M 2s
214200K .......... .......... .......... .......... .......... 80% 59.7M 2s
214250K .......... .......... .......... .......... .......... 80% 34.8M 2s
214300K .......... .......... .......... .......... .......... 80% 45.9M 2s
214350K .......... .......... .......... .......... .......... 80% 34.4M 2s
214400K .......... .......... .......... .......... .......... 80% 18.6M 2s
214450K .......... .......... .......... .......... .......... 80% 72.8M 2s
214500K .......... .......... .......... .......... .......... 80%  151M 2s
214550K .......... .......... .......... .......... .......... 80%  138M 2s
214600K .......... .......... .......... .......... .......... 80% 29.0M 2s
214650K .......... .......... .......... .......... .......... 80% 57.2M 2s
214700K .......... .......... .......... .......... .......... 80% 71.3M 2s
214750K .......... .......... .......... .......... .......... 80% 26.8M 2s
214800K .......... .......... .......... .......... .......... 80% 79.7M 2s
214850K .......... .......... .......... .......... .......... 80% 61.7M 2s
214900K .......... .......... .......... .......... .......... 80% 38.0M 2s
214950K .......... .......... .......... .......... .......... 80% 36.6M 2s
215000K .......... .......... .......... .......... .......... 80% 38.5M 2s
215050K .......... .......... .......... .......... .......... 80% 93.4M 2s
215100K .......... .......... .......... .......... .......... 80% 27.7M 2s
215150K .......... .......... .......... .......... .......... 80%  147M 2s
215200K .......... .......... .......... .......... .......... 80% 26.2M 2s
215250K .......... .......... .......... .......... .......... 80% 69.2M 2s
215300K .......... .......... .......... .......... .......... 81% 99.3M 2s
215350K .......... .......... .......... .......... .......... 81% 21.4M 2s
215400K .......... .......... .......... .......... .......... 81% 74.3M 2s
215450K .......... .......... .......... .......... .......... 81% 38.7M 2s
215500K .......... .......... .......... .......... .......... 81% 34.9M 2s
215550K .......... .......... .......... .......... .......... 81%  115M 2s
215600K .......... .......... .......... .......... .......... 81% 23.1M 2s
215650K .......... .......... .......... .......... .......... 81% 56.7M 2s
215700K .......... .......... .......... .......... .......... 81% 46.2M 2s
215750K .......... .......... .......... .......... .......... 81% 88.9M 2s
215800K .......... .......... .......... .......... .......... 81% 47.5M 2s
215850K .......... .......... .......... .......... .......... 81% 60.9M 2s
215900K .......... .......... .......... .......... .......... 81% 49.2M 2s
215950K .......... .......... .......... .......... .......... 81% 31.2M 2s
216000K .......... .......... .......... .......... .......... 81% 64.4M 2s
216050K .......... .......... .......... .......... .......... 81% 70.8M 2s
216100K .......... .......... .......... .......... .......... 81% 29.8M 2s
216150K .......... .......... .......... .......... .......... 81% 13.9M 2s
216200K .......... .......... .......... .......... .......... 81% 98.0M 2s
216250K .......... .......... .......... .......... .......... 81%  240M 2s
216300K .......... .......... .......... .......... .......... 81% 77.1M 2s
216350K .......... .......... .......... .......... .......... 81%  137M 2s
216400K .......... .......... .......... .......... .......... 81% 69.1M 2s
216450K .......... .......... .......... .......... .......... 81% 29.7M 2s
216500K .......... .......... .......... .......... .......... 81% 72.9M 2s
216550K .......... .......... .......... .......... .......... 81%  109M 2s
216600K .......... .......... .......... .......... .......... 81% 27.9M 2s
216650K .......... .......... .......... .......... .......... 81%  127M 2s
216700K .......... .......... .......... .......... .......... 81% 16.3M 2s
216750K .......... .......... .......... .......... .......... 81%  157M 2s
216800K .......... .......... .......... .......... .......... 81%  152M 2s
216850K .......... .......... .......... .......... .......... 81% 41.2M 2s
216900K .......... .......... .......... .......... .......... 81% 55.1M 2s
216950K .......... .......... .......... .......... .......... 81% 30.7M 2s
217000K .......... .......... .......... .......... .......... 81%  135M 2s
217050K .......... .......... .......... .......... .......... 81% 20.9M 2s
217100K .......... .......... .......... .......... .......... 81% 90.9M 2s
217150K .......... .......... .......... .......... .......... 81% 62.7M 2s
217200K .......... .......... .......... .......... .......... 81% 65.7M 2s
217250K .......... .......... .......... .......... .......... 81% 37.3M 2s
217300K .......... .......... .......... .......... .......... 81% 47.2M 2s
217350K .......... .......... .......... .......... .......... 81% 28.2M 2s
217400K .......... .......... .......... .......... .......... 81% 50.2M 2s
217450K .......... .......... .......... .......... .......... 81% 87.6M 2s
217500K .......... .......... .......... .......... .......... 81% 48.6M 2s
217550K .......... .......... .......... .......... .......... 81% 59.0M 2s
217600K .......... .......... .......... .......... .......... 81% 31.4M 2s
217650K .......... .......... .......... .......... .......... 81% 94.4M 2s
217700K .......... .......... .......... .......... .......... 81% 42.3M 2s
217750K .......... .......... .......... .......... .......... 81% 30.9M 2s
217800K .......... .......... .......... .......... .......... 81% 46.6M 2s
217850K .......... .......... .......... .......... .......... 81% 35.5M 2s
217900K .......... .......... .......... .......... .......... 81%  102M 2s
217950K .......... .......... .......... .......... .......... 82% 41.2M 2s
218000K .......... .......... .......... .......... .......... 82% 32.7M 2s
218050K .......... .......... .......... .......... .......... 82% 66.3M 2s
218100K .......... .......... .......... .......... .......... 82% 30.8M 2s
218150K .......... .......... .......... .......... .......... 82% 92.1M 2s
218200K .......... .......... .......... .......... .......... 82% 38.3M 2s
218250K .......... .......... .......... .......... .......... 82% 52.6M 2s
218300K .......... .......... .......... .......... .......... 82% 37.7M 2s
218350K .......... .......... .......... .......... .......... 82% 85.6M 2s
218400K .......... .......... .......... .......... .......... 82% 60.4M 2s
218450K .......... .......... .......... .......... .......... 82% 79.3M 2s
218500K .......... .......... .......... .......... .......... 82% 36.9M 2s
218550K .......... .......... .......... .......... .......... 82% 43.0M 2s
218600K .......... .......... .......... .......... .......... 82%  105M 2s
218650K .......... .......... .......... .......... .......... 82% 38.9M 2s
218700K .......... .......... .......... .......... .......... 82% 50.6M 2s
218750K .......... .......... .......... .......... .......... 82% 26.2M 2s
218800K .......... .......... .......... .......... .......... 82% 93.1M 2s
218850K .......... .......... .......... .......... .......... 82% 46.9M 2s
218900K .......... .......... .......... .......... .......... 82%  118M 2s
218950K .......... .......... .......... .......... .......... 82% 11.7M 2s
219000K .......... .......... .......... .......... .......... 82% 39.4M 2s
219050K .......... .......... .......... .......... .......... 82% 9.23M 2s
219100K .......... .......... .......... .......... .......... 82% 7.24M 2s
219150K .......... .......... .......... .......... .......... 82% 16.4M 2s
219200K .......... .......... .......... .......... .......... 82% 84.7M 2s
219250K .......... .......... .......... .......... .......... 82%  122M 2s
219300K .......... .......... .......... .......... .......... 82%  121M 2s
219350K .......... .......... .......... .......... .......... 82%  106M 2s
219400K .......... .......... .......... .......... .......... 82%  159M 2s
219450K .......... .......... .......... .......... .......... 82% 74.8M 2s
219500K .......... .......... .......... .......... .......... 82% 95.5M 2s
219550K .......... .......... .......... .......... .......... 82%  156M 2s
219600K .......... .......... .......... .......... .......... 82% 83.0M 2s
219650K .......... .......... .......... .......... .......... 82%  153M 2s
219700K .......... .......... .......... .......... .......... 82%  123M 2s
219750K .......... .......... .......... .......... .......... 82%  106M 2s
219800K .......... .......... .......... .......... .......... 82% 88.3M 2s
219850K .......... .......... .......... .......... .......... 82%  109M 2s
219900K .......... .......... .......... .......... .......... 82%  135M 2s
219950K .......... .......... .......... .......... .......... 82% 89.1M 2s
220000K .......... .......... .......... .......... .......... 82%  153M 2s
220050K .......... .......... .......... .......... .......... 82%  134M 2s
220100K .......... .......... .......... .......... .......... 82% 83.7M 2s
220150K .......... .......... .......... .......... .......... 82% 79.0M 2s
220200K .......... .......... .......... .......... .......... 82%  116M 2s
220250K .......... .......... .......... .......... .......... 82%  103M 2s
220300K .......... .......... .......... .......... .......... 82%  140M 2s
220350K .......... .......... .......... .......... .......... 82% 80.5M 2s
220400K .......... .......... .......... .......... .......... 82% 86.4M 2s
220450K .......... .......... .......... .......... .......... 82% 62.5M 2s
220500K .......... .......... .......... .......... .......... 82% 99.5M 2s
220550K .......... .......... .......... .......... .......... 82% 30.4M 2s
220600K .......... .......... .......... .......... .......... 83% 52.0M 2s
220650K .......... .......... .......... .......... .......... 83% 34.9M 2s
220700K .......... .......... .......... .......... .......... 83% 83.0M 2s
220750K .......... .......... .......... .......... .......... 83% 99.0M 2s
220800K .......... .......... .......... .......... .......... 83% 54.4M 2s
220850K .......... .......... .......... .......... .......... 83% 32.2M 2s
220900K .......... .......... .......... .......... .......... 83% 68.0M 2s
220950K .......... .......... .......... .......... .......... 83% 77.3M 2s
221000K .......... .......... .......... .......... .......... 83% 87.0M 2s
221050K .......... .......... .......... .......... .......... 83% 28.1M 2s
221100K .......... .......... .......... .......... .......... 83% 93.9M 2s
221150K .......... .......... .......... .......... .......... 83%  113M 2s
221200K .......... .......... .......... .......... .......... 83% 43.4M 2s
221250K .......... .......... .......... .......... .......... 83% 40.7M 2s
221300K .......... .......... .......... .......... .......... 83% 74.0M 2s
221350K .......... .......... .......... .......... .......... 83% 42.7M 2s
221400K .......... .......... .......... .......... .......... 83% 51.0M 2s
221450K .......... .......... .......... .......... .......... 83% 76.1M 2s
221500K .......... .......... .......... .......... .......... 83% 60.7M 2s
221550K .......... .......... .......... .......... .......... 83% 76.7M 2s
221600K .......... .......... .......... .......... .......... 83% 32.3M 2s
221650K .......... .......... .......... .......... .......... 83% 66.0M 2s
221700K .......... .......... .......... .......... .......... 83% 64.3M 2s
221750K .......... .......... .......... .......... .......... 83% 42.4M 2s
221800K .......... .......... .......... .......... .......... 83% 65.2M 2s
221850K .......... .......... .......... .......... .......... 83% 49.2M 2s
221900K .......... .......... .......... .......... .......... 83% 99.5M 2s
221950K .......... .......... .......... .......... .......... 83% 53.0M 2s
222000K .......... .......... .......... .......... .......... 83% 45.7M 2s
222050K .......... .......... .......... .......... .......... 83% 46.5M 2s
222100K .......... .......... .......... .......... .......... 83% 49.5M 2s
222150K .......... .......... .......... .......... .......... 83%  106M 2s
222200K .......... .......... .......... .......... .......... 83% 47.2M 2s
222250K .......... .......... .......... .......... .......... 83% 68.9M 2s
222300K .......... .......... .......... .......... .......... 83% 42.7M 2s
222350K .......... .......... .......... .......... .......... 83% 56.3M 2s
222400K .......... .......... .......... .......... .......... 83% 75.3M 2s
222450K .......... .......... .......... .......... .......... 83% 44.3M 2s
222500K .......... .......... .......... .......... .......... 83% 64.5M 2s
222550K .......... .......... .......... .......... .......... 83% 38.6M 2s
222600K .......... .......... .......... .......... .......... 83% 64.9M 2s
222650K .......... .......... .......... .......... .......... 83%  126M 2s
222700K .......... .......... .......... .......... .......... 83% 43.7M 2s
222750K .......... .......... .......... .......... .......... 83% 19.8M 2s
222800K .......... .......... .......... .......... .......... 83%  149M 2s
222850K .......... .......... .......... .......... .......... 83% 93.1M 2s
222900K .......... .......... .......... .......... .......... 83%  103M 2s
222950K .......... .......... .......... .......... .......... 83% 13.4M 2s
223000K .......... .......... .......... .......... .......... 83% 73.3M 2s
223050K .......... .......... .......... .......... .......... 83%  126M 2s
223100K .......... .......... .......... .......... .......... 83%  108M 2s
223150K .......... .......... .......... .......... .......... 83%  140M 2s
223200K .......... .......... .......... .......... .......... 83% 42.9M 2s
223250K .......... .......... .......... .......... .......... 84%  128M 2s
223300K .......... .......... .......... .......... .......... 84%  208M 2s
223350K .......... .......... .......... .......... .......... 84%  104M 2s
223400K .......... .......... .......... .......... .......... 84% 23.2M 2s
223450K .......... .......... .......... .......... .......... 84% 80.6M 2s
223500K .......... .......... .......... .......... .......... 84% 80.8M 2s
223550K .......... .......... .......... .......... .......... 84%  153M 2s
223600K .......... .......... .......... .......... .......... 84% 24.7M 2s
223650K .......... .......... .......... .......... .......... 84%  114M 2s
223700K .......... .......... .......... .......... .......... 84% 71.8M 2s
223750K .......... .......... .......... .......... .......... 84% 17.6M 2s
223800K .......... .......... .......... .......... .......... 84%  109M 2s
223850K .......... .......... .......... .......... .......... 84%  102M 2s
223900K .......... .......... .......... .......... .......... 84%  136M 2s
223950K .......... .......... .......... .......... .......... 84% 39.9M 2s
224000K .......... .......... .......... .......... .......... 84% 28.1M 2s
224050K .......... .......... .......... .......... .......... 84% 83.7M 2s
224100K .......... .......... .......... .......... .......... 84% 56.4M 2s
224150K .......... .......... .......... .......... .......... 84% 23.0M 2s
224200K .......... .......... .......... .......... .......... 84% 50.4M 2s
224250K .......... .......... .......... .......... .......... 84%  118M 2s
224300K .......... .......... .......... .......... .......... 84% 72.4M 2s
224350K .......... .......... .......... .......... .......... 84% 42.0M 2s
224400K .......... .......... .......... .......... .......... 84% 92.0M 2s
224450K .......... .......... .......... .......... .......... 84%  106M 2s
224500K .......... .......... .......... .......... .......... 84% 98.9M 2s
224550K .......... .......... .......... .......... .......... 84% 72.0M 2s
224600K .......... .......... .......... .......... .......... 84% 55.7M 2s
224650K .......... .......... .......... .......... .......... 84% 92.5M 2s
224700K .......... .......... .......... .......... .......... 84% 31.0M 2s
224750K .......... .......... .......... .......... .......... 84%  155M 2s
224800K .......... .......... .......... .......... .......... 84% 40.7M 2s
224850K .......... .......... .......... .......... .......... 84% 96.8M 2s
224900K .......... .......... .......... .......... .......... 84% 36.9M 2s
224950K .......... .......... .......... .......... .......... 84% 43.3M 2s
225000K .......... .......... .......... .......... .......... 84% 93.2M 2s
225050K .......... .......... .......... .......... .......... 84%  128M 2s
225100K .......... .......... .......... .......... .......... 84% 35.4M 2s
225150K .......... .......... .......... .......... .......... 84% 50.2M 2s
225200K .......... .......... .......... .......... .......... 84% 51.7M 2s
225250K .......... .......... .......... .......... .......... 84%  161M 2s
225300K .......... .......... .......... .......... .......... 84% 35.0M 2s
225350K .......... .......... .......... .......... .......... 84% 50.1M 2s
225400K .......... .......... .......... .......... .......... 84% 58.6M 2s
225450K .......... .......... .......... .......... .......... 84%  123M 2s
225500K .......... .......... .......... .......... .......... 84% 38.6M 2s
225550K .......... .......... .......... .......... .......... 84% 53.2M 2s
225600K .......... .......... .......... .......... .......... 84% 73.9M 2s
225650K .......... .......... .......... .......... .......... 84% 46.1M 2s
225700K .......... .......... .......... .......... .......... 84% 61.7M 2s
225750K .......... .......... .......... .......... .......... 84% 48.2M 2s
225800K .......... .......... .......... .......... .......... 84% 93.3M 2s
225850K .......... .......... .......... .......... .......... 84% 34.1M 2s
225900K .......... .......... .......... .......... .......... 85%  124M 2s
225950K .......... .......... .......... .......... .......... 85% 38.5M 2s
226000K .......... .......... .......... .......... .......... 85%  113M 2s
226050K .......... .......... .......... .......... .......... 85% 34.9M 1s
226100K .......... .......... .......... .......... .......... 85% 55.9M 1s
226150K .......... .......... .......... .......... .......... 85% 76.6M 1s
226200K .......... .......... .......... .......... .......... 85% 42.8M 1s
226250K .......... .......... .......... .......... .......... 85% 57.4M 1s
226300K .......... .......... .......... .......... .......... 85% 48.9M 1s
226350K .......... .......... .......... .......... .......... 85% 60.6M 1s
226400K .......... .......... .......... .......... .......... 85% 83.1M 1s
226450K .......... .......... .......... .......... .......... 85% 41.1M 1s
226500K .......... .......... .......... .......... .......... 85% 56.8M 1s
226550K .......... .......... .......... .......... .......... 85% 62.4M 1s
226600K .......... .......... .......... .......... .......... 85% 45.9M 1s
226650K .......... .......... .......... .......... .......... 85% 84.2M 1s
226700K .......... .......... .......... .......... .......... 85% 48.9M 1s
226750K .......... .......... .......... .......... .......... 85% 52.2M 1s
226800K .......... .......... .......... .......... .......... 85% 53.4M 1s
226850K .......... .......... .......... .......... .......... 85% 34.0M 1s
226900K .......... .......... .......... .......... .......... 85% 80.0M 1s
226950K .......... .......... .......... .......... .......... 85% 63.2M 1s
227000K .......... .......... .......... .......... .......... 85% 58.6M 1s
227050K .......... .......... .......... .......... .......... 85% 64.0M 1s
227100K .......... .......... .......... .......... .......... 85% 61.8M 1s
227150K .......... .......... .......... .......... .......... 85% 57.1M 1s
227200K .......... .......... .......... .......... .......... 85% 45.1M 1s
227250K .......... .......... .......... .......... .......... 85% 45.5M 1s
227300K .......... .......... .......... .......... .......... 85% 69.5M 1s
227350K .......... .......... .......... .......... .......... 85% 59.6M 1s
227400K .......... .......... .......... .......... .......... 85% 51.4M 1s
227450K .......... .......... .......... .......... .......... 85% 44.3M 1s
227500K .......... .......... .......... .......... .......... 85% 56.8M 1s
227550K .......... .......... .......... .......... .......... 85% 83.9M 1s
227600K .......... .......... .......... .......... .......... 85% 44.8M 1s
227650K .......... .......... .......... .......... .......... 85% 48.3M 1s
227700K .......... .......... .......... .......... .......... 85% 43.0M 1s
227750K .......... .......... .......... .......... .......... 85% 63.1M 1s
227800K .......... .......... .......... .......... .......... 85% 69.5M 1s
227850K .......... .......... .......... .......... .......... 85% 56.5M 1s
227900K .......... .......... .......... .......... .......... 85% 40.2M 1s
227950K .......... .......... .......... .......... .......... 85% 78.1M 1s
228000K .......... .......... .......... .......... .......... 85% 32.5M 1s
228050K .......... .......... .......... .......... .......... 85%  122M 1s
228100K .......... .......... .......... .......... .......... 85% 72.9M 1s
228150K .......... .......... .......... .......... .......... 85% 37.9M 1s
228200K .......... .......... .......... .......... .......... 85% 62.1M 1s
228250K .......... .......... .......... .......... .......... 85% 38.5M 1s
228300K .......... .......... .......... .......... .......... 85% 20.5M 1s
228350K .......... .......... .......... .......... .......... 85% 70.8M 1s
228400K .......... .......... .......... .......... .......... 85%  176M 1s
228450K .......... .......... .......... .......... .......... 85%  145M 1s
228500K .......... .......... .......... .......... .......... 85%  163M 1s
228550K .......... .......... .......... .......... .......... 86% 49.9M 1s
228600K .......... .......... .......... .......... .......... 86% 40.1M 1s
228650K .......... .......... .......... .......... .......... 86% 55.2M 1s
228700K .......... .......... .......... .......... .......... 86% 28.3M 1s
228750K .......... .......... .......... .......... .......... 86% 96.8M 1s
228800K .......... .......... .......... .......... .......... 86% 82.8M 1s
228850K .......... .......... .......... .......... .......... 86% 28.2M 1s
228900K .......... .......... .......... .......... .......... 86% 18.6M 1s
228950K .......... .......... .......... .......... .......... 86% 22.4M 1s
229000K .......... .......... .......... .......... .......... 86% 29.3M 1s
229050K .......... .......... .......... .......... .......... 86% 24.6M 1s
229100K .......... .......... .......... .......... .......... 86% 38.5M 1s
229150K .......... .......... .......... .......... .......... 86% 44.7M 1s
229200K .......... .......... .......... .......... .......... 86% 35.4M 1s
229250K .......... .......... .......... .......... .......... 86% 44.3M 1s
229300K .......... .......... .......... .......... .......... 86% 33.6M 1s
229350K .......... .......... .......... .......... .......... 86% 50.2M 1s
229400K .......... .......... .......... .......... .......... 86% 22.0M 1s
229450K .......... .......... .......... .......... .......... 86% 22.7M 1s
229500K .......... .......... .......... .......... .......... 86% 37.9M 1s
229550K .......... .......... .......... .......... .......... 86% 62.4M 1s
229600K .......... .......... .......... .......... .......... 86% 49.6M 1s
229650K .......... .......... .......... .......... .......... 86%  116M 1s
229700K .......... .......... .......... .......... .......... 86% 96.5M 1s
229750K .......... .......... .......... .......... .......... 86%  102M 1s
229800K .......... .......... .......... .......... .......... 86% 30.0M 1s
229850K .......... .......... .......... .......... .......... 86% 49.1M 1s
229900K .......... .......... .......... .......... .......... 86% 79.6M 1s
229950K .......... .......... .......... .......... .......... 86% 48.0M 1s
230000K .......... .......... .......... .......... .......... 86%  141M 1s
230050K .......... .......... .......... .......... .......... 86%  151M 1s
230100K .......... .......... .......... .......... .......... 86% 63.0M 1s
230150K .......... .......... .......... .......... .......... 86%  198M 1s
230200K .......... .......... .......... .......... .......... 86% 23.6M 1s
230250K .......... .......... .......... .......... .......... 86% 92.6M 1s
230300K .......... .......... .......... .......... .......... 86% 70.0M 1s
230350K .......... .......... .......... .......... .......... 86% 28.6M 1s
230400K .......... .......... .......... .......... .......... 86% 64.3M 1s
230450K .......... .......... .......... .......... .......... 86% 88.2M 1s
230500K .......... .......... .......... .......... .......... 86% 46.3M 1s
230550K .......... .......... .......... .......... .......... 86% 21.3M 1s
230600K .......... .......... .......... .......... .......... 86% 29.5M 1s
230650K .......... .......... .......... .......... .......... 86% 43.2M 1s
230700K .......... .......... .......... .......... .......... 86% 32.1M 1s
230750K .......... .......... .......... .......... .......... 86% 86.7M 1s
230800K .......... .......... .......... .......... .......... 86% 36.9M 1s
230850K .......... .......... .......... .......... .......... 86%  102M 1s
230900K .......... .......... .......... .......... .......... 86% 45.3M 1s
230950K .......... .......... .......... .......... .......... 86% 35.3M 1s
231000K .......... .......... .......... .......... .......... 86% 26.0M 1s
231050K .......... .......... .......... .......... .......... 86% 68.1M 1s
231100K .......... .......... .......... .......... .......... 86% 46.2M 1s
231150K .......... .......... .......... .......... .......... 86% 45.9M 1s
231200K .......... .......... .......... .......... .......... 86% 27.4M 1s
231250K .......... .......... .......... .......... .......... 87% 44.8M 1s
231300K .......... .......... .......... .......... .......... 87% 56.4M 1s
231350K .......... .......... .......... .......... .......... 87% 65.8M 1s
231400K .......... .......... .......... .......... .......... 87% 70.6M 1s
231450K .......... .......... .......... .......... .......... 87%  156M 1s
231500K .......... .......... .......... .......... .......... 87%  265M 1s
231550K .......... .......... .......... .......... .......... 87% 36.7M 1s
231600K .......... .......... .......... .......... .......... 87% 57.5M 1s
231650K .......... .......... .......... .......... .......... 87% 88.6M 1s
231700K .......... .......... .......... .......... .......... 87% 59.3M 1s
231750K .......... .......... .......... .......... .......... 87%  164M 1s
231800K .......... .......... .......... .......... .......... 87% 92.9M 1s
231850K .......... .......... .......... .......... .......... 87% 79.7M 1s
231900K .......... .......... .......... .......... .......... 87% 23.3M 1s
231950K .......... .......... .......... .......... .......... 87% 75.9M 1s
232000K .......... .......... .......... .......... .......... 87% 26.7M 1s
232050K .......... .......... .......... .......... .......... 87% 37.2M 1s
232100K .......... .......... .......... .......... .......... 87% 28.6M 1s
232150K .......... .......... .......... .......... .......... 87% 36.0M 1s
232200K .......... .......... .......... .......... .......... 87% 33.2M 1s
232250K .......... .......... .......... .......... .......... 87%  237M 1s
232300K .......... .......... .......... .......... .......... 87%  205M 1s
232350K .......... .......... .......... .......... .......... 87%  179M 1s
232400K .......... .......... .......... .......... .......... 87%  151M 1s
232450K .......... .......... .......... .......... .......... 87%  149M 1s
232500K .......... .......... .......... .......... .......... 87%  199M 1s
232550K .......... .......... .......... .......... .......... 87%  251M 1s
232600K .......... .......... .......... .......... .......... 87%  180M 1s
232650K .......... .......... .......... .......... .......... 87%  276M 1s
232700K .......... .......... .......... .......... .......... 87% 87.4M 1s
232750K .......... .......... .......... .......... .......... 87%  198M 1s
232800K .......... .......... .......... .......... .......... 87% 63.0M 1s
232850K .......... .......... .......... .......... .......... 87% 42.6M 1s
232900K .......... .......... .......... .......... .......... 87% 33.7M 1s
232950K .......... .......... .......... .......... .......... 87% 44.2M 1s
233000K .......... .......... .......... .......... .......... 87%  134M 1s
233050K .......... .......... .......... .......... .......... 87% 43.4M 1s
233100K .......... .......... .......... .......... .......... 87% 31.6M 1s
233150K .......... .......... .......... .......... .......... 87% 50.1M 1s
233200K .......... .......... .......... .......... .......... 87% 44.4M 1s
233250K .......... .......... .......... .......... .......... 87% 99.0M 1s
233300K .......... .......... .......... .......... .......... 87% 31.6M 1s
233350K .......... .......... .......... .......... .......... 87% 44.1M 1s
233400K .......... .......... .......... .......... .......... 87% 53.9M 1s
233450K .......... .......... .......... .......... .......... 87% 28.1M 1s
233500K .......... .......... .......... .......... .......... 87%  157M 1s
233550K .......... .......... .......... .......... .......... 87% 26.3M 1s
233600K .......... .......... .......... .......... .......... 87% 21.4M 1s
233650K .......... .......... .......... .......... .......... 87% 89.4M 1s
233700K .......... .......... .......... .......... .......... 87% 54.9M 1s
233750K .......... .......... .......... .......... .......... 87% 64.8M 1s
233800K .......... .......... .......... .......... .......... 87% 71.5M 1s
233850K .......... .......... .......... .......... .......... 87% 23.0M 1s
233900K .......... .......... .......... .......... .......... 88% 51.6M 1s
233950K .......... .......... .......... .......... .......... 88% 50.6M 1s
234000K .......... .......... .......... .......... .......... 88% 70.7M 1s
234050K .......... .......... .......... .......... .......... 88% 37.6M 1s
234100K .......... .......... .......... .......... .......... 88% 31.9M 1s
234150K .......... .......... .......... .......... .......... 88% 25.6M 1s
234200K .......... .......... .......... .......... .......... 88% 34.9M 1s
234250K .......... .......... .......... .......... .......... 88% 45.4M 1s
234300K .......... .......... .......... .......... .......... 88% 29.2M 1s
234350K .......... .......... .......... .......... .......... 88% 28.8M 1s
234400K .......... .......... .......... .......... .......... 88% 66.9M 1s
234450K .......... .......... .......... .......... .......... 88% 73.6M 1s
234500K .......... .......... .......... .......... .......... 88% 20.9M 1s
234550K .......... .......... .......... .......... .......... 88% 29.0M 1s
234600K .......... .......... .......... .......... .......... 88% 23.5M 1s
234650K .......... .......... .......... .......... .......... 88% 36.9M 1s
234700K .......... .......... .......... .......... .......... 88% 34.3M 1s
234750K .......... .......... .......... .......... .......... 88% 91.2M 1s
234800K .......... .......... .......... .......... .......... 88%  137M 1s
234850K .......... .......... .......... .......... .......... 88% 76.9M 1s
234900K .......... .......... .......... .......... .......... 88%  104M 1s
234950K .......... .......... .......... .......... .......... 88% 73.7M 1s
235000K .......... .......... .......... .......... .......... 88%  126M 1s
235050K .......... .......... .......... .......... .......... 88%  115M 1s
235100K .......... .......... .......... .......... .......... 88% 65.0M 1s
235150K .......... .......... .......... .......... .......... 88% 93.4M 1s
235200K .......... .......... .......... .......... .......... 88% 66.2M 1s
235250K .......... .......... .......... .......... .......... 88% 94.7M 1s
235300K .......... .......... .......... .......... .......... 88% 82.5M 1s
235350K .......... .......... .......... .......... .......... 88%  115M 1s
235400K .......... .......... .......... .......... .......... 88% 54.1M 1s
235450K .......... .......... .......... .......... .......... 88% 25.1M 1s
235500K .......... .......... .......... .......... .......... 88% 33.7M 1s
235550K .......... .......... .......... .......... .......... 88% 32.8M 1s
235600K .......... .......... .......... .......... .......... 88% 38.4M 1s
235650K .......... .......... .......... .......... .......... 88% 68.4M 1s
235700K .......... .......... .......... .......... .......... 88%  237M 1s
235750K .......... .......... .......... .......... .......... 88% 69.9M 1s
235800K .......... .......... .......... .......... .......... 88%  127M 1s
235850K .......... .......... .......... .......... .......... 88% 44.1M 1s
235900K .......... .......... .......... .......... .......... 88% 44.5M 1s
235950K .......... .......... .......... .......... .......... 88% 31.3M 1s
236000K .......... .......... .......... .......... .......... 88% 45.8M 1s
236050K .......... .......... .......... .......... .......... 88% 48.7M 1s
236100K .......... .......... .......... .......... .......... 88% 73.2M 1s
236150K .......... .......... .......... .......... .......... 88% 32.6M 1s
236200K .......... .......... .......... .......... .......... 88% 46.7M 1s
236250K .......... .......... .......... .......... .......... 88% 56.8M 1s
236300K .......... .......... .......... .......... .......... 88%  126M 1s
236350K .......... .......... .......... .......... .......... 88% 28.1M 1s
236400K .......... .......... .......... .......... .......... 88% 49.5M 1s
236450K .......... .......... .......... .......... .......... 88% 38.8M 1s
236500K .......... .......... .......... .......... .......... 88% 34.9M 1s
236550K .......... .......... .......... .......... .......... 89% 73.9M 1s
236600K .......... .......... .......... .......... .......... 89% 45.4M 1s
236650K .......... .......... .......... .......... .......... 89% 53.2M 1s
236700K .......... .......... .......... .......... .......... 89% 30.3M 1s
236750K .......... .......... .......... .......... .......... 89% 88.8M 1s
236800K .......... .......... .......... .......... .......... 89% 59.2M 1s
236850K .......... .......... .......... .......... .......... 89% 19.9M 1s
236900K .......... .......... .......... .......... .......... 89% 88.5M 1s
236950K .......... .......... .......... .......... .......... 89% 72.0M 1s
237000K .......... .......... .......... .......... .......... 89% 75.5M 1s
237050K .......... .......... .......... .......... .......... 89% 51.9M 1s
237100K .......... .......... .......... .......... .......... 89% 26.8M 1s
237150K .......... .......... .......... .......... .......... 89% 73.0M 1s
237200K .......... .......... .......... .......... .......... 89% 39.2M 1s
237250K .......... .......... .......... .......... .......... 89%  118M 1s
237300K .......... .......... .......... .......... .......... 89% 31.8M 1s
237350K .......... .......... .......... .......... .......... 89% 46.4M 1s
237400K .......... .......... .......... .......... .......... 89% 47.0M 1s
237450K .......... .......... .......... .......... .......... 89% 28.6M 1s
237500K .......... .......... .......... .......... .......... 89% 71.7M 1s
237550K .......... .......... .......... .......... .......... 89% 46.1M 1s
237600K .......... .......... .......... .......... .......... 89% 57.8M 1s
237650K .......... .......... .......... .......... .......... 89% 31.8M 1s
237700K .......... .......... .......... .......... .......... 89% 49.4M 1s
237750K .......... .......... .......... .......... .......... 89% 79.1M 1s
237800K .......... .......... .......... .......... .......... 89% 45.7M 1s
237850K .......... .......... .......... .......... .......... 89% 33.7M 1s
237900K .......... .......... .......... .......... .......... 89% 54.7M 1s
237950K .......... .......... .......... .......... .......... 89% 81.0M 1s
238000K .......... .......... .......... .......... .......... 89% 50.2M 1s
238050K .......... .......... .......... .......... .......... 89% 30.5M 1s
238100K .......... .......... .......... .......... .......... 89% 39.4M 1s
238150K .......... .......... .......... .......... .......... 89% 63.4M 1s
238200K .......... .......... .......... .......... .......... 89% 92.2M 1s
238250K .......... .......... .......... .......... .......... 89% 30.5M 1s
238300K .......... .......... .......... .......... .......... 89% 50.7M 1s
238350K .......... .......... .......... .......... .......... 89% 45.9M 1s
238400K .......... .......... .......... .......... .......... 89%  129M 1s
238450K .......... .......... .......... .......... .......... 89% 25.5M 1s
238500K .......... .......... .......... .......... .......... 89% 61.9M 1s
238550K .......... .......... .......... .......... .......... 89% 50.2M 1s
238600K .......... .......... .......... .......... .......... 89% 30.8M 1s
238650K .......... .......... .......... .......... .......... 89%  105M 1s
238700K .......... .......... .......... .......... .......... 89% 42.7M 1s
238750K .......... .......... .......... .......... .......... 89% 53.4M 1s
238800K .......... .......... .......... .......... .......... 89% 31.2M 1s
238850K .......... .......... .......... .......... .......... 89% 23.4M 1s
238900K .......... .......... .......... .......... .......... 89%  114M 1s
238950K .......... .......... .......... .......... .......... 89%  124M 1s
239000K .......... .......... .......... .......... .......... 89% 80.4M 1s
239050K .......... .......... .......... .......... .......... 89% 32.9M 1s
239100K .......... .......... .......... .......... .......... 89% 46.8M 1s
239150K .......... .......... .......... .......... .......... 89%  107M 1s
239200K .......... .......... .......... .......... .......... 90% 48.7M 1s
239250K .......... .......... .......... .......... .......... 90% 31.3M 1s
239300K .......... .......... .......... .......... .......... 90% 31.8M 1s
239350K .......... .......... .......... .......... .......... 90% 26.6M 1s
239400K .......... .......... .......... .......... .......... 90% 45.3M 1s
239450K .......... .......... .......... .......... .......... 90% 26.8M 1s
239500K .......... .......... .......... .......... .......... 90% 87.6M 1s
239550K .......... .......... .......... .......... .......... 90% 40.2M 1s
239600K .......... .......... .......... .......... .......... 90% 40.9M 1s
239650K .......... .......... .......... .......... .......... 90%  204M 1s
239700K .......... .......... .......... .......... .......... 90%  141M 1s
239750K .......... .......... .......... .......... .......... 90%  111M 1s
239800K .......... .......... .......... .......... .......... 90% 50.4M 1s
239850K .......... .......... .......... .......... .......... 90% 84.1M 1s
239900K .......... .......... .......... .......... .......... 90% 48.7M 1s
239950K .......... .......... .......... .......... .......... 90% 30.7M 1s
240000K .......... .......... .......... .......... .......... 90% 49.8M 1s
240050K .......... .......... .......... .......... .......... 90% 81.7M 1s
240100K .......... .......... .......... .......... .......... 90% 13.8M 1s
240150K .......... .......... .......... .......... .......... 90% 51.6M 1s
240200K .......... .......... .......... .......... .......... 90% 28.1M 1s
240250K .......... .......... .......... .......... .......... 90%  111M 1s
240300K .......... .......... .......... .......... .......... 90%  162M 1s
240350K .......... .......... .......... .......... .......... 90% 96.8M 1s
240400K .......... .......... .......... .......... .......... 90%  125M 1s
240450K .......... .......... .......... .......... .......... 90% 47.4M 1s
240500K .......... .......... .......... .......... .......... 90% 36.4M 1s
240550K .......... .......... .......... .......... .......... 90% 79.4M 1s
240600K .......... .......... .......... .......... .......... 90% 47.1M 1s
240650K .......... .......... .......... .......... .......... 90% 53.7M 1s
240700K .......... .......... .......... .......... .......... 90% 30.2M 1s
240750K .......... .......... .......... .......... .......... 90% 31.9M 1s
240800K .......... .......... .......... .......... .......... 90% 54.9M 1s
240850K .......... .......... .......... .......... .......... 90% 24.9M 1s
240900K .......... .......... .......... .......... .......... 90% 79.4M 1s
240950K .......... .......... .......... .......... .......... 90% 69.6M 1s
241000K .......... .......... .......... .......... .......... 90% 44.8M 1s
241050K .......... .......... .......... .......... .......... 90% 37.6M 1s
241100K .......... .......... .......... .......... .......... 90% 57.1M 1s
241150K .......... .......... .......... .......... .......... 90% 47.1M 1s
241200K .......... .......... .......... .......... .......... 90% 35.5M 1s
241250K .......... .......... .......... .......... .......... 90% 31.9M 1s
241300K .......... .......... .......... .......... .......... 90% 34.7M 1s
241350K .......... .......... .......... .......... .......... 90% 41.7M 1s
241400K .......... .......... .......... .......... .......... 90% 84.9M 1s
241450K .......... .......... .......... .......... .......... 90% 79.6M 1s
241500K .......... .......... .......... .......... .......... 90% 56.9M 1s
241550K .......... .......... .......... .......... .......... 90% 41.2M 1s
241600K .......... .......... .......... .......... .......... 90% 48.7M 1s
241650K .......... .......... .......... .......... .......... 90% 48.5M 1s
241700K .......... .......... .......... .......... .......... 90% 79.5M 1s
241750K .......... .......... .......... .......... .......... 90% 54.7M 1s
241800K .......... .......... .......... .......... .......... 90% 51.1M 1s
241850K .......... .......... .......... .......... .......... 91% 35.1M 1s
241900K .......... .......... .......... .......... .......... 91% 64.4M 1s
241950K .......... .......... .......... .......... .......... 91% 53.1M 1s
242000K .......... .......... .......... .......... .......... 91% 68.1M 1s
242050K .......... .......... .......... .......... .......... 91% 38.1M 1s
242100K .......... .......... .......... .......... .......... 91% 67.2M 1s
242150K .......... .......... .......... .......... .......... 91%  154M 1s
242200K .......... .......... .......... .......... .......... 91%  112M 1s
242250K .......... .......... .......... .......... .......... 91%  150M 1s
242300K .......... .......... .......... .......... .......... 91%  247M 1s
242350K .......... .......... .......... .......... .......... 91% 42.2M 1s
242400K .......... .......... .......... .......... .......... 91%  143M 1s
242450K .......... .......... .......... .......... .......... 91% 40.0M 1s
242500K .......... .......... .......... .......... .......... 91% 50.5M 1s
242550K .......... .......... .......... .......... .......... 91%  100M 1s
242600K .......... .......... .......... .......... .......... 91% 20.0M 1s
242650K .......... .......... .......... .......... .......... 91% 28.9M 1s
242700K .......... .......... .......... .......... .......... 91% 90.9M 1s
242750K .......... .......... .......... .......... .......... 91% 80.8M 1s
242800K .......... .......... .......... .......... .......... 91%  118M 1s
242850K .......... .......... .......... .......... .......... 91%  108M 1s
242900K .......... .......... .......... .......... .......... 91% 55.9M 1s
242950K .......... .......... .......... .......... .......... 91% 85.4M 1s
243000K .......... .......... .......... .......... .......... 91% 46.5M 1s
243050K .......... .......... .......... .......... .......... 91% 53.6M 1s
243100K .......... .......... .......... .......... .......... 91% 29.5M 1s
243150K .......... .......... .......... .......... .......... 91%  102M 1s
243200K .......... .......... .......... .......... .......... 91%  106M 1s
243250K .......... .......... .......... .......... .......... 91% 53.1M 1s
243300K .......... .......... .......... .......... .......... 91% 45.0M 1s
243350K .......... .......... .......... .......... .......... 91% 43.7M 1s
243400K .......... .......... .......... .......... .......... 91%  114M 1s
243450K .......... .......... .......... .......... .......... 91% 42.8M 1s
243500K .......... .......... .......... .......... .......... 91% 56.6M 1s
243550K .......... .......... .......... .......... .......... 91% 51.6M 1s
243600K .......... .......... .......... .......... .......... 91%  112M 1s
243650K .......... .......... .......... .......... .......... 91% 33.1M 1s
243700K .......... .......... .......... .......... .......... 91% 45.1M 1s
243750K .......... .......... .......... .......... .......... 91% 75.1M 1s
243800K .......... .......... .......... .......... .......... 91% 41.5M 1s
243850K .......... .......... .......... .......... .......... 91% 86.1M 1s
243900K .......... .......... .......... .......... .......... 91% 43.9M 1s
243950K .......... .......... .......... .......... .......... 91% 97.9M 1s
244000K .......... .......... .......... .......... .......... 91% 37.2M 1s
244050K .......... .......... .......... .......... .......... 91% 51.7M 1s
244100K .......... .......... .......... .......... .......... 91% 39.0M 1s
244150K .......... .......... .......... .......... .......... 91% 42.9M 1s
244200K .......... .......... .......... .......... .......... 91% 48.8M 1s
244250K .......... .......... .......... .......... .......... 91%  180M 1s
244300K .......... .......... .......... .......... .......... 91% 67.5M 1s
244350K .......... .......... .......... .......... .......... 91% 47.3M 1s
244400K .......... .......... .......... .......... .......... 91% 43.7M 1s
244450K .......... .......... .......... .......... .......... 91% 62.6M 1s
244500K .......... .......... .......... .......... .......... 92% 45.9M 1s
244550K .......... .......... .......... .......... .......... 92% 86.6M 1s
244600K .......... .......... .......... .......... .......... 92% 43.7M 1s
244650K .......... .......... .......... .......... .......... 92% 65.5M 1s
244700K .......... .......... .......... .......... .......... 92% 42.4M 1s
244750K .......... .......... .......... .......... .......... 92% 51.0M 1s
244800K .......... .......... .......... .......... .......... 92% 60.6M 1s
244850K .......... .......... .......... .......... .......... 92% 66.0M 1s
244900K .......... .......... .......... .......... .......... 92% 53.0M 1s
244950K .......... .......... .......... .......... .......... 92% 41.1M 1s
245000K .......... .......... .......... .......... .......... 92% 35.2M 1s
245050K .......... .......... .......... .......... .......... 92% 49.9M 1s
245100K .......... .......... .......... .......... .......... 92% 62.8M 1s
245150K .......... .......... .......... .......... .......... 92% 69.4M 1s
245200K .......... .......... .......... .......... .......... 92%  107M 1s
245250K .......... .......... .......... .......... .......... 92% 37.5M 1s
245300K .......... .......... .......... .......... .......... 92% 71.3M 1s
245350K .......... .......... .......... .......... .......... 92% 97.5M 1s
245400K .......... .......... .......... .......... .......... 92% 43.9M 1s
245450K .......... .......... .......... .......... .......... 92% 59.1M 1s
245500K .......... .......... .......... .......... .......... 92% 65.2M 1s
245550K .......... .......... .......... .......... .......... 92% 48.6M 1s
245600K .......... .......... .......... .......... .......... 92% 47.8M 1s
245650K .......... .......... .......... .......... .......... 92% 82.6M 1s
245700K .......... .......... .......... .......... .......... 92% 42.8M 1s
245750K .......... .......... .......... .......... .......... 92% 97.5M 1s
245800K .......... .......... .......... .......... .......... 92% 45.3M 1s
245850K .......... .......... .......... .......... .......... 92% 46.4M 1s
245900K .......... .......... .......... .......... .......... 92% 53.1M 1s
245950K .......... .......... .......... .......... .......... 92% 46.8M 1s
246000K .......... .......... .......... .......... .......... 92%  114M 1s
246050K .......... .......... .......... .......... .......... 92% 48.0M 1s
246100K .......... .......... .......... .......... .......... 92% 36.6M 1s
246150K .......... .......... .......... .......... .......... 92% 65.4M 1s
246200K .......... .......... .......... .......... .......... 92% 84.3M 1s
246250K .......... .......... .......... .......... .......... 92% 56.1M 1s
246300K .......... .......... .......... .......... .......... 92% 47.5M 1s
246350K .......... .......... .......... .......... .......... 92% 20.9M 1s
246400K .......... .......... .......... .......... .......... 92%  153M 1s
246450K .......... .......... .......... .......... .......... 92%  113M 1s
246500K .......... .......... .......... .......... .......... 92%  133M 1s
246550K .......... .......... .......... .......... .......... 92% 44.0M 1s
246600K .......... .......... .......... .......... .......... 92% 52.2M 1s
246650K .......... .......... .......... .......... .......... 92% 88.0M 1s
246700K .......... .......... .......... .......... .......... 92% 49.1M 1s
246750K .......... .......... .......... .......... .......... 92% 49.0M 1s
246800K .......... .......... .......... .......... .......... 92% 51.1M 1s
246850K .......... .......... .......... .......... .......... 92% 47.5M 1s
246900K .......... .......... .......... .......... .......... 92%  121M 1s
246950K .......... .......... .......... .......... .......... 92% 43.9M 1s
247000K .......... .......... .......... .......... .......... 92% 42.9M 1s
247050K .......... .......... .......... .......... .......... 92% 53.8M 1s
247100K .......... .......... .......... .......... .......... 92% 52.0M 1s
247150K .......... .......... .......... .......... .......... 92% 94.6M 1s
247200K .......... .......... .......... .......... .......... 93% 44.7M 1s
247250K .......... .......... .......... .......... .......... 93% 46.4M 1s
247300K .......... .......... .......... .......... .......... 93% 27.2M 1s
247350K .......... .......... .......... .......... .......... 93%  147M 1s
247400K .......... .......... .......... .......... .......... 93%  210M 1s
247450K .......... .......... .......... .......... .......... 93% 46.9M 1s
247500K .......... .......... .......... .......... .......... 93% 52.4M 1s
247550K .......... .......... .......... .......... .......... 93% 46.5M 1s
247600K .......... .......... .......... .......... .......... 93%  110M 1s
247650K .......... .......... .......... .......... .......... 93% 50.1M 1s
247700K .......... .......... .......... .......... .......... 93% 47.8M 1s
247750K .......... .......... .......... .......... .......... 93% 30.8M 1s
247800K .......... .......... .......... .......... .......... 93% 67.0M 1s
247850K .......... .......... .......... .......... .......... 93% 90.0M 1s
247900K .......... .......... .......... .......... .......... 93% 42.8M 1s
247950K .......... .......... .......... .......... .......... 93% 50.9M 1s
248000K .......... .......... .......... .......... .......... 93% 58.0M 1s
248050K .......... .......... .......... .......... .......... 93% 63.1M 1s
248100K .......... .......... .......... .......... .......... 93% 83.9M 1s
248150K .......... .......... .......... .......... .......... 93% 55.2M 1s
248200K .......... .......... .......... .......... .......... 93% 42.9M 1s
248250K .......... .......... .......... .......... .......... 93% 54.1M 1s
248300K .......... .......... .......... .......... .......... 93%  110M 1s
248350K .......... .......... .......... .......... .......... 93% 22.1M 1s
248400K .......... .......... .......... .......... .......... 93%  172M 1s
248450K .......... .......... .......... .......... .......... 93% 48.7M 1s
248500K .......... .......... .......... .......... .......... 93% 88.2M 1s
248550K .......... .......... .......... .......... .......... 93%  125M 1s
248600K .......... .......... .......... .......... .......... 93% 35.1M 1s
248650K .......... .......... .......... .......... .......... 93% 45.9M 1s
248700K .......... .......... .......... .......... .......... 93% 74.4M 1s
248750K .......... .......... .......... .......... .......... 93% 44.7M 1s
248800K .......... .......... .......... .......... .......... 93% 50.0M 1s
248850K .......... .......... .......... .......... .......... 93% 70.8M 1s
248900K .......... .......... .......... .......... .......... 93% 50.7M 1s
248950K .......... .......... .......... .......... .......... 93% 35.9M 1s
249000K .......... .......... .......... .......... .......... 93% 53.8M 1s
249050K .......... .......... .......... .......... .......... 93% 81.5M 1s
249100K .......... .......... .......... .......... .......... 93% 87.7M 1s
249150K .......... .......... .......... .......... .......... 93% 55.8M 1s
249200K .......... .......... .......... .......... .......... 93% 51.7M 1s
249250K .......... .......... .......... .......... .......... 93% 38.5M 1s
249300K .......... .......... .......... .......... .......... 93% 38.2M 1s
249350K .......... .......... .......... .......... .......... 93% 52.8M 1s
249400K .......... .......... .......... .......... .......... 93% 86.3M 1s
249450K .......... .......... .......... .......... .......... 93% 51.1M 1s
249500K .......... .......... .......... .......... .......... 93%  131M 1s
249550K .......... .......... .......... .......... .......... 93% 60.1M 1s
249600K .......... .......... .......... .......... .......... 93% 44.6M 1s
249650K .......... .......... .......... .......... .......... 93% 70.8M 1s
249700K .......... .......... .......... .......... .......... 93% 50.5M 1s
249750K .......... .......... .......... .......... .......... 93%  101M 1s
249800K .......... .......... .......... .......... .......... 93% 32.5M 1s
249850K .......... .......... .......... .......... .......... 94% 36.6M 1s
249900K .......... .......... .......... .......... .......... 94% 51.4M 1s
249950K .......... .......... .......... .......... .......... 94% 35.0M 1s
250000K .......... .......... .......... .......... .......... 94% 64.6M 1s
250050K .......... .......... .......... .......... .......... 94% 64.5M 1s
250100K .......... .......... .......... .......... .......... 94% 58.2M 1s
250150K .......... .......... .......... .......... .......... 94% 30.1M 1s
250200K .......... .......... .......... .......... .......... 94% 36.6M 1s
250250K .......... .......... .......... .......... .......... 94% 39.2M 1s
250300K .......... .......... .......... .......... .......... 94%  161M 1s
250350K .......... .......... .......... .......... .......... 94%  132M 1s
250400K .......... .......... .......... .......... .......... 94% 59.0M 1s
250450K .......... .......... .......... .......... .......... 94% 82.4M 1s
250500K .......... .......... .......... .......... .......... 94% 52.3M 1s
250550K .......... .......... .......... .......... .......... 94% 32.7M 1s
250600K .......... .......... .......... .......... .......... 94% 50.5M 1s
250650K .......... .......... .......... .......... .......... 94% 53.9M 1s
250700K .......... .......... .......... .......... .......... 94% 72.5M 1s
250750K .......... .......... .......... .......... .......... 94% 51.6M 1s
250800K .......... .......... .......... .......... .......... 94% 33.4M 1s
250850K .......... .......... .......... .......... .......... 94% 56.5M 1s
250900K .......... .......... .......... .......... .......... 94% 94.6M 1s
250950K .......... .......... .......... .......... .......... 94% 42.2M 1s
251000K .......... .......... .......... .......... .......... 94% 28.1M 1s
251050K .......... .......... .......... .......... .......... 94% 83.2M 1s
251100K .......... .......... .......... .......... .......... 94% 41.6M 1s
251150K .......... .......... .......... .......... .......... 94% 93.3M 1s
251200K .......... .......... .......... .......... .......... 94% 26.2M 1s
251250K .......... .......... .......... .......... .......... 94% 44.9M 1s
251300K .......... .......... .......... .......... .......... 94% 39.1M 1s
251350K .......... .......... .......... .......... .......... 94% 32.8M 1s
251400K .......... .......... .......... .......... .......... 94% 47.0M 1s
251450K .......... .......... .......... .......... .......... 94% 49.6M 1s
251500K .......... .......... .......... .......... .......... 94% 92.5M 1s
251550K .......... .......... .......... .......... .......... 94% 55.3M 1s
251600K .......... .......... .......... .......... .......... 94% 47.8M 1s
251650K .......... .......... .......... .......... .......... 94%  198M 1s
251700K .......... .......... .......... .......... .......... 94% 52.3M 1s
251750K .......... .......... .......... .......... .......... 94% 48.2M 1s
251800K .......... .......... .......... .......... .......... 94% 49.7M 1s
251850K .......... .......... .......... .......... .......... 94% 89.3M 0s
251900K .......... .......... .......... .......... .......... 94% 49.6M 0s
251950K .......... .......... .......... .......... .......... 94% 33.7M 0s
252000K .......... .......... .......... .......... .......... 94% 32.1M 0s
252050K .......... .......... .......... .......... .......... 94% 36.9M 0s
252100K .......... .......... .......... .......... .......... 94%  122M 0s
252150K .......... .......... .......... .......... .......... 94%  113M 0s
252200K .......... .......... .......... .......... .......... 94% 48.6M 0s
252250K .......... .......... .......... .......... .......... 94% 31.6M 0s
252300K .......... .......... .......... .......... .......... 94%  119M 0s
252350K .......... .......... .......... .......... .......... 94% 43.1M 0s
252400K .......... .......... .......... .......... .......... 94% 51.5M 0s
252450K .......... .......... .......... .......... .......... 94% 44.4M 0s
252500K .......... .......... .......... .......... .......... 95% 33.7M 0s
252550K .......... .......... .......... .......... .......... 95%  109M 0s
252600K .......... .......... .......... .......... .......... 95% 47.9M 0s
252650K .......... .......... .......... .......... .......... 95% 44.1M 0s
252700K .......... .......... .......... .......... .......... 95% 47.3M 0s
252750K .......... .......... .......... .......... .......... 95% 32.2M 0s
252800K .......... .......... .......... .......... .......... 95%  103M 0s
252850K .......... .......... .......... .......... .......... 95% 47.2M 0s
252900K .......... .......... .......... .......... .......... 95% 45.6M 0s
252950K .......... .......... .......... .......... .......... 95% 58.2M 0s
253000K .......... .......... .......... .......... .......... 95% 30.5M 0s
253050K .......... .......... .......... .......... .......... 95% 91.2M 0s
253100K .......... .......... .......... .......... .......... 95% 28.4M 0s
253150K .......... .......... .......... .......... .......... 95% 39.8M 0s
253200K .......... .......... .......... .......... .......... 95% 47.4M 0s
253250K .......... .......... .......... .......... .......... 95% 40.6M 0s
253300K .......... .......... .......... .......... .......... 95% 35.7M 0s
253350K .......... .......... .......... .......... .......... 95% 40.5M 0s
253400K .......... .......... .......... .......... .......... 95%  108M 0s
253450K .......... .......... .......... .......... .......... 95% 48.7M 0s
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265800K ......                                                100%  112M=9.2s

2024-06-25 22:59:15 (28.2 MB/s) - ‘ESPbeta.tgz’ saved [272186226/272186226]

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

ESP runtime AutoConfigurator

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


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

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

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

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

+ source /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=LINUX64
++ ESP_ARCH=LINUX64
++ export ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad
++ ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad
++ export CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export CASARCH=.
++ CASARCH=.
++ export CASREV=7.8
++ CASREV=7.8
++ export PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/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/7.8/LINUX64/EngSketchPad/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/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/7.8/LINUX64/EngSketchPad/pyESP:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ export AFLR_ARCH=Linux-x86-64
++ AFLR_ARCH=Linux-x86-64
++ '[' -z /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib: ']'
++ export LD_LIBRARY_PATH=/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ LD_LIBRARY_PATH=/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ export UDUNITS2_XML_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ export CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ export TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ export 'SLUGS_START=firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/SLUGS/Slugs.html &'
++ SLUGS_START='firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/SLUGS/Slugs.html &'
++ export 'ESP_START=firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/ESP/ESP.html &'
++ ESP_START='firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/ESP/ESP.html &'
++ export 'WV_START=firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/wvClient/wv.html &'
++ WV_START='firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/wvClient/wv.html &'
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src
+ make
(cd EGADS/src; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/src'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/LINUX64
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/LINUX64
cp -p ../include/LINUX64 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/LINUX64
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/STANALYZER.make
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/STANALYZER.make
cp -p ../include/STANALYZER.make /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/STANALYZER.make
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.h
cp -p ../include/egads.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads_dot.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads_dot.h
cp -p ../include/egads_dot.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads_dot.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.inc
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.inc
cp -p ../include/egads.inc /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.inc
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsErrors.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsErrors.h
cp -p ../include/egadsErrors.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsErrors.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTypes.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTypes.h
cp -p ../include/egadsTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTypes.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/emp.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/emp.h
cp -p ../include/emp.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/emp.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/prm.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/prm.h
cp -p ../include/prm.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/prm.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.h
cp -p ../include/wsserver.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.inc
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.inc
cp -p ../include/wsserver.inc /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.inc
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsss.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsss.h
cp -p ../include/wsss.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsss.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTris.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTris.h
cp -p egadsTris.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTris.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineFit.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineFit.h
cp -p egadsSplineFit.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineFit.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineVels.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineVels.h
cp -p egadsSplineVels.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineVels.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsf90.inc
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsf90.inc
cp -p ../include/egadsf90.inc /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsf90.inc
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealD.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Lazy.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealD_Lazy.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Trad.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealD_Trad.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealS.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Lazy.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealS_Lazy.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Trad.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealS_Trad.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/always_inline.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/always_inline.h
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsGeom.cpp -o ./egadsGeom.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsHLevel.cpp -o ./egadsHLevel.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsTopo.cpp -o ./egadsTopo.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsCopy.cpp -o ./egadsCopy.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsSpline.cpp -o ./egadsSpline.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsIO.cpp -o ./egadsIO.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsSplineFit.cpp -o ./egadsSplineFit.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsSkinning.cpp -o ./egadsSkinning.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsTessSens.cpp -o ./egadsTessSens.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 OCC/BRepLib_FuseEdges.cpp -o ./BRepLib_FuseEdges.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsBase.c -o ./egadsBase.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsMemory.c -o ./egadsMemory.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsAttrs.c -o ./egadsAttrs.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsTess.c -o ./egadsTess.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsTessInp.c -o ./egadsTessInp.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsTris.c -o ./egadsTris.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsQuads.c -o ./egadsQuads.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsFit.c -o ./egadsFit.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsRobust.c -o ./egadsRobust.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsSBO.c -o ./egadsSBO.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap prmCfit.c -o ./prmCfit.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap prmGrid.c -o ./prmGrid.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap prmUV.c -o ./prmUV.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsExport.c -o ./egadsExport.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsEffect.c -o ./egadsEffect.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsSolids.c -o ./egadsSolids.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include ../util/emp.c \
	-o ./emp.o
g++ -g  -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \
	../util/evaluate.c -o ./evaluate.o
g++ -g  -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \
	../util/rational.c -o ./rational.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include -I../util \
	../util/regQuads.c -o ./regQuads.o
g++ -g  -o ./SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp
./SurrealD1

SurrealD1_test_suite Complete!

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

SurrealD4_test_suite Complete!

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

SurrealS1_test_suite Complete!

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

SurrealS4_test_suite Complete!

make -C ../util
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/util'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 uvmap/main/uvmap.c -Iuvmap \
	-o ./uvmap.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_bnd_adj.c -o ./uvmap_bnd_adj.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibfibf.c -o ./uvmap_ibfibf.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_message.c -o ./uvmap_message.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibfin.c -o ./uvmap_ibfin.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_read.c -o ./uvmap_read.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_iccin.c -o ./uvmap_iccin.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_add.c -o ./uvmap_add.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_cpu_message.c -o ./uvmap_cpu_message.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapFindUV.c -o ./EG_uvmapFindUV.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapTest.c -o ./EG_uvmapTest.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_inibe.c -o ./uvmap_inibe.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_version.c -o ./uvmap_version.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_inl_uv_bnd.c -o ./uvmap_inl_uv_bnd.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_chk_edge_ratio.c -o ./uvmap_chk_edge_ratio.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_struct_tasks.c -o ./uvmap_struct_tasks.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmap_Read.c -o ./EG_uvmap_Read.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_idibe.c -o ./uvmap_idibe.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapStructFree.c -o ./EG_uvmapStructFree.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapGen.c -o ./EG_uvmapGen.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_write.c -o ./uvmap_write.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibeibe.c -o ./uvmap_ibeibe.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_chk_area_uv.c -o ./uvmap_chk_area_uv.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_norm_uv.c -o ./uvmap_norm_uv.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_iccibe.c -o ./uvmap_iccibe.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_malloc.c -o ./uvmap_malloc.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_gen_uv.c -o ./uvmap_gen_uv.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_to_egads.c -o ./uvmap_to_egads.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmap_Write.c -o ./EG_uvmap_Write.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_test.c -o ./uvmap_test.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_mben_disc.c -o ./uvmap_mben_disc.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_find_uv.c -o ./uvmap_find_uv.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_gen.c -o ./uvmap_gen.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_solve.c -o ./uvmap_solve.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_from_egads.c -o ./uvmap_from_egads.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 egadsUVmap.c -Iuvmap \
	-o ./egadsUVmap.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a ./egadsUVmap.o uvmap_cpu_message.o uvmap_ibfibf.o uvmap_message.o uvmap_version.o uvmap_gen_uv.o uvmap_inl_uv_bnd.o EG_uvmap_Read.o uvmap_chk_edge_ratio.o uvmap_idibe.o uvmap_write.o uvmap_ibeibe.o uvmap_chk_area_uv.o uvmap_gen.o uvmap_malloc.o uvmap_to_egads.o EG_uvmap_Write.o uvmap_iccibe.o EG_uvmapGen.o EG_uvmapTest.o uvmap_read.o uvmap_ibfin.o uvmap_iccin.o uvmap_add.o EG_uvmapFindUV.o uvmap_struct_tasks.o uvmap_bnd_adj.o EG_uvmapStructFree.o uvmap_inibe.o uvmap_norm_uv.o uvmap_test.o uvmap_mben_disc.o uvmap_find_uv.o uvmap_solve.o uvmap_from_egads.o;  )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a
gcc -g  -o ./uvmap.exe ./uvmap.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -luvmap -lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/util'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegads.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegads.so
(cd .; gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegads.so \
	egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o   egadsSplineFit.o egadsSkinning.o egadsTessSens.o  BRepLib_FuseEdges.o  egadsBase.o egadsMemory.o egadsAttrs.o  egadsTess.o   egadsTessInp.o egadsTris.o egadsQuads.o  egadsFit.o    egadsRobust.o egadsSBO.o prmCfit.o   prmGrid.o     prmUV.o       egadsExport.o egadsEffect.o egadsSolids.o emp.o evaluate.o rational.o regQuads.o \
	-L/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -pthread -lm -lstdc++ -lrt )
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadstatic.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadstatic.a
cp /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadstatic.a
(cd .; \
	ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadstatic.a egadsBase.o egadsMemory.o egadsAttrs.o  egadsTess.o   egadsTessInp.o egadsTris.o egadsQuads.o  egadsFit.o    egadsRobust.o egadsSBO.o prmCfit.o   prmGrid.o     prmUV.o       egadsExport.o egadsEffect.o egadsSolids.o egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o   egadsSplineFit.o egadsSkinning.o egadsTessSens.o  BRepLib_FuseEdges.o  emp.o \
	evaluate.o rational.o regQuads.o;  )
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsBase.c -o ./fgadsBase.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsMemory.c -o ./fgadsMemory.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsAttrs.c -o ./fgadsAttrs.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsTess.c -o ./fgadsTess.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsHLevel.c -o ./fgadsHLevel.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsGeom.c -o ./fgadsGeom.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsTopo.c -o ./fgadsTopo.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libfgads.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libfgads.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libfgads.a fgadsBase.o fgadsMemory.o fgadsAttrs.o  fgadsTess.o   fgadsHLevel.o fgadsGeom.o fgadsTopo.o;  )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libfgads.a
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a emp.o;  )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a
 *** EGADS Build Complete! ***
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/src'
(cd EGADS/lite; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/lite'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteBase.c -o ./liteBase.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteMemory.c -o ./liteMemory.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteGeom.c -o ./liteGeom.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteTopo.c -o ./liteTopo.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteAttrs.c -o ./liteAttrs.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteImport.c -o ./liteImport.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteString.c -o ./liteString.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                ../src/egadsTess.c -o ./liteTess.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                ../src/egadsTris.c -o ./liteTris.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src \
                ../src/egadsQuads.c -o ./liteQuads.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                -I../util ../src/egadsTessInp.c -o ./liteTessInp.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 ../src/egadsRobust.c \
	-o ./egadsRobust.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLINUX64 -I../include ../util/emp.c \
	-o ./emp.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
	../util/evaluate.c -o ./evaLite.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE ../util/rational.c \
	-o ./ratLite.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I../util \
	../util/regQuads.c -o ./liteRegQuads.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                ../src/egadsEffect.c -o ./liteEffect.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                -I../util/uvmap liteUVmap.c -o ./liteUVmap.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslite.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslite.so
(cd .; gcc -g  -shared -Wl,-no-undefined \
	-o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslite.so liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o liteTess.o liteTris.o \
	liteQuads.o liteTessInp.o egadsRobust.o emp.o evaLite.o \
	ratLite.o liteRegQuads.o liteEffect.o liteUVmap.o \
	-lpthread -lm )
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslitestatic.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslitestatic.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslitestatic.a liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o \
                liteTess.o liteTris.o liteQuads.o liteTessInp.o egadsRobust.o \
	emp.o evaLite.o ratLite.o liteRegQuads.o liteEffect.o \
	liteUVmap.o ;  )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslitestatic.a
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/lite'
(cd wvServer; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/wvServer'
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 map.cpp -o ./map.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include base64-decode.c -o ./base64-decode.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include handshake.c -o ./handshake.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include client-handshake.c -o ./client-handshake.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include libwebsockets.c -o ./libwebsockets.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include extension-deflate-stream.c -o ./extension-deflate-stream.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include md5.c -o ./md5.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include extension-x-google-mux.c -o ./extension-x-google-mux.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include parsers.c -o ./parsers.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include extension.c -o ./extension.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include sha-1.c -o ./sha-1.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include server.c -o ./server.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include wv.c -o ./wv.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include browserMessage.c -o ./browserMessage.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include fwv.c -o ./fwv.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a map.o base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o \
	./fwv.o;  )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -DSTANDALONE server.c \
	-I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -o ./servertest.o
g++ -g  -o ./server ./servertest.o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a  \
	-lpthread -lz -lm
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.so
(cd .; g++ -g  -shared -Wl,-no-undefined \
	-o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.so base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o map.o -lz -lpthread)
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/wvServer'
(cd EGADS/examples; make -f egads2cart.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include egads2cart.c \
	-o ./egads2cart.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/egads2cart ./egads2cart.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads \
	-lrt -lm
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vCurvature.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include vCurvature.c -o ./vCurvature.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vCurvature ./vCurvature.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legads -lrt
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vGeom.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include vGeom.c -o ./vGeom.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vGeom ./vGeom.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legads \
	-lrt
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vTess.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include vTess.c -o ./vTess.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include ../util/retessFaces.c \
	-o ./retessFaces.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vTesstatic ./vTess.o ./retessFaces.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legadstatic -L/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -pthread -lm \
	-lpthread -lz -lrt -lm
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vTess ./vTess.o ./retessFaces.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legads -lrt
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
(cd OpenCSM; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/OpenCSM'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. serveCSM.c -o ./serveCSM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. OpenCSM.c -o ./OpenCSM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udp.c -o ./udp.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. tim.c -o ./tim.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libocsm.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libocsm.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libocsm.so ./OpenCSM.o ./udp.o ./tim.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads -lwsserver -ldl -lrt -lm
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/serveCSM ./serveCSM.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. serveESP.c -o ./serveESP.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/serveESP ./serveESP.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. sensCSM.c -o ./sensCSM.o
gcc -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/sensCSM ./sensCSM.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lrt -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBezier.c -o ./udpBezier.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bezier.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bezier.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bezier.so ./udpBezier.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBiconvex.c -o ./udpBiconvex.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/biconvex.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/biconvex.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/biconvex.so ./udpBiconvex.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBox.c -o ./udpBox.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/box.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/box.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/box.so ./udpBox.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBspline.c -o ./udpBspline.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bspline.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bspline.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bspline.so ./udpBspline.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCatmull.c -o ./udfCatmull.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/catmull.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/catmull.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/catmull.so ./udfCatmull.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCompare.c -o ./udfCompare.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/compare.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/compare.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/compare.so ./udfCompare.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCreateBEM.c -o ./udfCreateBEM.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createBEM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createBEM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createBEM.so ./udfCreateBEM.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCreatePoly.c -o ./udfCreatePoly.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createPoly.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createPoly.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createPoly.so ./udfCreatePoly.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpCsm.c -o ./udpCsm.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/csm.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/csm.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/csm.so ./udpCsm.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfDeform.c -o ./udfDeform.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/deform.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/deform.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/deform.so ./udfDeform.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfDroop.c -o ./udfDroop.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/droop.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/droop.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/droop.so ./udfDroop.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfDumpPmtrs.c -o ./udfDumpPmtrs.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/dumpPmtrs.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/dumpPmtrs.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/dumpPmtrs.so ./udfDumpPmtrs.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfEditAttr.c -o ./udfEditAttr.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/editAttr.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/editAttr.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/editAttr.so ./udfEditAttr.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpEllipse.c -o ./udpEllipse.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ellipse.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ellipse.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ellipse.so ./udpEllipse.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpEqn2body.c -o ./udpEqn2body.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/eqn2body.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/eqn2body.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/eqn2body.so ./udpEqn2body.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpFitcurve.c -o ./udpFitcurve.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fitcurve.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fitcurve.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fitcurve.so ./udpFitcurve.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfFlend.c -o ./udfFlend.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flend.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flend.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flend.so ./udfFlend.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpFreeform.c -o ./udpFreeform.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/freeform.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/freeform.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/freeform.so ./udpFreeform.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfGanged.c -o ./udfGanged.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ganged.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ganged.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ganged.so ./udfGanged.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfGuide.c -o ./udfGuide.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/guide.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/guide.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/guide.so ./udfGuide.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpHex.c -o ./udpHex.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hex.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hex.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hex.so ./udpHex.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpImport.c -o ./udpImport.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/import.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/import.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/import.so ./udpImport.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpKulfan.c -o ./udpKulfan.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/kulfan.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/kulfan.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/kulfan.so ./udpKulfan.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfLinalg.c -o ./udfLinalg.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/linalg.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/linalg.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/linalg.so ./udfLinalg.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfMatchBodys.c -o ./udfMatchBodys.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/matchBodys.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/matchBodys.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/matchBodys.so ./udfMatchBodys.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfMechanism.c -o ./udfMechanism.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mechanism.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mechanism.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mechanism.so ./udfMechanism.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpNaca.c -o ./udpNaca.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca.so ./udpNaca.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfNaca6mc.c -o ./udfNaca6mc.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca6mc.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca6mc.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca6mc.so ./udfNaca6mc.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfNacelle.c -o ./udfNacelle.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nacelle.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nacelle.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nacelle.so ./udfNacelle.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpNurbbody.c -o ./udpNurbbody.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nurbbody.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nurbbody.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nurbbody.so ./udpNurbbody.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfNuscale.c -o ./udfNuscale.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nuscale.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nuscale.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nuscale.so ./udfNuscale.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfOffset.c -o ./udfOffset.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/offset.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/offset.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/offset.so ./udfOffset.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpParabaloid.c -o ./udpParabaloid.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parabaloid.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parabaloid.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parabaloid.so ./udpParabaloid.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpParsec.cpp -o ./udpParsec.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parsec.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parsec.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parsec.so ./udpParsec.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpPod.c -o ./udpPod.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pod.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pod.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pod.so ./udpPod.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpPoly.c -o ./udpPoly.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/poly.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/poly.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/poly.so ./udpPoly.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfPrintBbox.c -o ./udfPrintBbox.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBbox.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBbox.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBbox.so ./udfPrintBbox.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfPrintBrep.c -o ./udfPrintBrep.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBrep.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBrep.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBrep.so ./udfPrintBrep.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfPrintEgo.c -o ./udfPrintEgo.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printEgo.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printEgo.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printEgo.so ./udfPrintEgo.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpProp.c -o ./udpProp.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/prop.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/prop.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/prop.so ./udpProp.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpRadwaf.c -o ./udpRadwaf.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/radwaf.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/radwaf.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/radwaf.so ./udpRadwaf.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpSample.c -o ./udpSample.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sample.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sample.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sample.so ./udpSample.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpSew.c -o ./udpSew.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sew.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sew.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sew.so ./udpSew.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfShadow.c -o ./udfShadow.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/shadow.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/shadow.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/shadow.so ./udfShadow.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfSlices.c -o ./udfSlices.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slices.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slices.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slices.so ./udfSlices.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpStag.c -o ./udpStag.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stag.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stag.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stag.so ./udpStag.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfStiffener.c -o ./udfStiffener.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stiffener.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stiffener.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stiffener.so ./udfStiffener.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpSupell.c -o ./udpSupell.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/supell.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/supell.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/supell.so ./udpSupell.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfTester1.c -o ./udfTester1.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester1.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester1.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester1.so ./udfTester1.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpTester2.c -o ./udpTester2.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester2.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester2.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester2.so ./udpTester2.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpVsp3.c -o ./udpVsp3.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vsp3.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vsp3.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vsp3.so ./udpVsp3.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpWaffle.c -o ./udpWaffle.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/waffle.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/waffle.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/waffle.so ./udpWaffle.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfWarp.c -o ./udfWarp.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/warp.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/warp.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/warp.so ./udfWarp.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. eggPDT2.c -o ./eggPDT2.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/PDT2.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/PDT2.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/PDT2.so ./eggPDT2.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpNaca456.c -o ./udpNaca456.o
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer naca456.f90 -o ./naca456.o -J .
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca456.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca456.so
gfortran -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca456.so ./udpNaca456.o ./naca456.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm 
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timEreped.c -o ./timEreped.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ereped.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ereped.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ereped.so ./timEreped.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timMitten.c -o ./timMitten.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mitten.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mitten.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mitten.so ./timMitten.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timPlotter.c -o ./timPlotter.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plotter.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plotter.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plotter.so ./timPlotter.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timPlugs.c -o ./timPlugs.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plugs.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plugs.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plugs.so ./timPlugs.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timSlugs.c -o ./timSlugs.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slugs.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slugs.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slugs.so ./timSlugs.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timVspSetup.c -o ./timVspSetup.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vspSetup.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vspSetup.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vspSetup.so ./timVspSetup.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/OpenCSM.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/OpenCSM.h
cp -p OpenCSM.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/OpenCSM.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/common.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/common.h
cp -p common.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/common.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udp.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udp.h
cp -p udp.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udp.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/esp.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/esp.h
cp -p esp.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/esp.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/tim.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/tim.h
cp -p tim.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/tim.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egg.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egg.h
cp -p egg.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egg.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.h
cp -p udpUtilities.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.c
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.c
cp -p udpUtilities.c /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.c
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/OpenCSM'
(cd Slugs; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/Slugs'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. Slugs.c -o ./Slugs.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. Fitter.c \
	-o ./Fitter.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. RedBlackTree.c \
	-o ./RedBlackTree.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. Tessellate.c \
	-o ./Tessellate.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/Slugs ./Slugs.o ./Fitter.o ./RedBlackTree.o \
	./Tessellate.o -lrt -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legads \
	-lpthread -lz -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. TestFit.c -o ./TestFit.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/TestFit ./TestFit.o ./Fitter.o -lrt -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads \
	-lpthread -lz -lm
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/Slugs'
(cd CAPS; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS'
/bin/cp Cart3D/X86_64_GCC/libc3dio.a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libc3dio.a
/bin/cp Cart3D/X86_64_GCC/libCart3D.a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libCart3D.a
/bin/cp Executables/LINUX64/avl /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/avl
/bin/cp Executables/LINUX64/pplot /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/pplot
/bin/cp Executables/LINUX64/pxplot /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/pxplot
/bin/cp Executables/LINUX64/xfoil /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/xfoil
/bin/cp Executables/LINUX64/mastros.exe /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/mastros.exe
/bin/cp Executables/LINUX64/ASTRO.D01 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/ASTRO.D01
/bin/cp Executables/LINUX64/ASTRO.IDX /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/ASTRO.IDX
/bin/cp Executables/LINUX64/mses /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/mses
/bin/cp Executables/LINUX64/mset /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/mset
/bin/cp udunits/include/*.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include
/bin/cp udunits/LINUX64/libudunits2.so /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib
ln -sf libudunits2.so /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libudunits2.so.0
/bin/cp Libraries/LINUX64/aflr2AIM.so /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/aflr2AIM.so
/bin/cp Libraries/LINUX64/aflr3AIM.so /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/aflr3AIM.so
/bin/cp Libraries/LINUX64/aflr4AIM.so /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/aflr4AIM.so
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS'
(cd CAPS/src; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/src'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/caps.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/caps.h
cp -p ../include/caps.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/caps.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsErrors.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsErrors.h
cp -p ../include/capsErrors.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsErrors.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsTypes.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsTypes.h
cp -p ../include/capsTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsTypes.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimUtil.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimUtil.h
cp -p ../include/aimUtil.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimUtil.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimMesh.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimMesh.h
cp -p ../include/aimMesh.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimMesh.h
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../include \
	-I/usr/include/udunits2 aimUtil.c -o ./aimUtil.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include \
	-I/usr/include/udunits2 aimTransferUtil.c \
	-o ./aimTransferUtil.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../include \
	aimMesh.c -o ./aimMesh.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libaimUtil.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libaimUtil.a
ar -rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libaimUtil.a ./aimUtil.o ./aimMesh.o \
	./aimTransferUtil.o 
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libaimUtil.a
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsBase.c -o ./capsBase.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsAnalysis.c -o ./capsAnalysis.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsApprox.c -o ./capsApprox.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsAttr.c -o ./capsAttr.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsAIM.c -o ./capsAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsBound.c -o ./capsBound.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsProblem.c -o ./capsProblem.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsValue.c -o ./capsValue.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsUnits.c -o ./capsUnits.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 conjGrad.c -o ./conjGrad.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsFunIDs.c -o ./capsFunIDs.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsChkInpt.c -o ./capsChkInpt.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 printObject.c -o ./printObject.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcaps.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcaps.so
(cd .; gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcaps.so \
		capsBase.o   capsAnalysis.o capsApprox.o capsAttr.o  capsAIM.o capsBound.o  capsProblem.o  capsValue.o  capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o  printObject.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -ludunits2 -locsm -legads -ldl \
		-lrt -lm )
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcapsstatic.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcapsstatic.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcapsstatic.a capsBase.o   capsAnalysis.o capsApprox.o capsAttr.o  capsAIM.o capsBound.o  capsProblem.o  capsValue.o  capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o  printObject.o )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcapsstatic.a
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include testingAIM.c \
	-o ./testingAIM.o
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so
rm: cannot remove '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so': No such file or directory
make[1]: [Makefile:23: /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so] Error 1 (ignored)
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so ./testingAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include testingWriter.c \
	-o ./testingWriter.o
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so
rm: cannot remove '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so': No such file or directory
make[1]: [Makefile:33: /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so] Error 1 (ignored)
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so ./testingWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -ldl -lrt -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include phaseUtil.c \
	-o ./phaseUtil.o
gcc -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/phaseUtil ./phaseUtil.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -ludunits2 -locsm -legads -ldl -lrt -lm
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/src'
(cd ../CAPSexamples; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples'
(make -C cCAPS -f aeroelastic_SU2.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o
gcc -g  -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include avlTest.c -o ./avlTest.o
gcc -g  -o ./avlTest ./avlTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include awaveTest.c -o ./awaveTest.o
gcc -g  -o ./awaveTest ./awaveTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include frictionTest.c -o ./frictionTest.o
gcc -g  -o ./frictionTest ./frictionTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include fun3dAFLR2Test.c -o ./fun3dAFLR2Test.o
gcc -g  -o ./fun3dAFLR2Test ./fun3dAFLR2Test.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include fun3dTetgenTest.c -o ./fun3dTetgenTest.o
gcc -g  -o ./fun3dTetgenTest ./fun3dTetgenTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include aeroelasticTest.c -o ./aeroelasticTest.o
gcc -g  -o ./aeroelasticTest ./aeroelasticTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f hsm.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmTest.c -o ./hsmTest.o   
gcc -g  -o ./hsmTest ./hsmTest.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmSimplePlateTest.c -o ./hsmSimplePlateTest.o  
gcc -g  -o ./hsmSimplePlateTest ./hsmSimplePlateTest.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmCantileverPlateTest.c -o ./hsmCantileverPlateTest.o  
gcc -g  -o ./hsmCantileverPlateTest ./hsmCantileverPlateTest.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmJoinedPlateTest.c -o ./hsmJoinedPlateTest.o  
gcc -g  -o ./hsmJoinedPlateTest ./hsmJoinedPlateTest.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include interferenceTest.c \
	-o ./interferenceTest.o   
gcc -g  -o ./interferenceTest ./interferenceTest.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include msesTest.c -o ./msesTest.o
gcc -g  -o ./msesTest ./msesTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f mystran.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include mystranTest.c -o ./mystranTest.o   
gcc -g  -o ./mystranTest ./mystranTest.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include pointwiseTest.c -o ./pointwiseTest.o
gcc -g  -o ./pointwiseTest ./pointwiseTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples'
(cd CAPS/aim; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim'
make -C utils
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/utils'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython attrUtils.c -o ./attrUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython meshUtils.c -o ./meshUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cfdUtils.c -o ./cfdUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython miscUtils.c -o ./miscUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython feaUtils.c -o ./feaUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython vlmUtils.c -o ./vlmUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranCards.c -o ./nastranCards.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranUtils.c -o ./nastranUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython tecplotUtils.c -o ./tecplotUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython arrayUtils.c -o ./arrayUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython deprecateUtils.c -o ./deprecateUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cardUtils.c -o ./cardUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython jsonUtils.c -o ./jsonUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cython/nastranOP2Reader.c -o ./nastranOP2Reader.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. vlmSpanSpace.cpp -o ./vlmSpanSpace.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libutils.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libutils.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libutils.a attrUtils.o meshUtils.o cfdUtils.o miscUtils.o feaUtils.o vlmUtils.o nastranCards.o nastranUtils.o tecplotUtils.o arrayUtils.o deprecateUtils.o cardUtils.o jsonUtils.o nastranOP2Reader.o vlmSpanSpace.o )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libutils.a
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils
cp -p -f attrUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/attrUtils.h
cp -p -f nastranCards.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/nastranCards.h
cp -p -f cfdTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cfdTypes.h
cp -p -f arrayUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/arrayUtils.h
cp -p -f meshUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/meshUtils.h
cp -p -f feaTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/feaTypes.h
cp -p -f miscUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/miscUtils.h
cp -p -f meshTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/meshTypes.h
cp -p -f attrTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/attrTypes.h
cp -p -f vlmTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/vlmTypes.h
cp -p -f feaUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/feaUtils.h
cp -p -f cfdUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cfdUtils.h
cp -p -f vlmUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/vlmUtils.h
cp -p -f cardTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cardTypes.h
cp -p -f jsonUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/jsonUtils.h
cp -p -f nastranUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/nastranUtils.h
cp -p -f deprecateUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/deprecateUtils.h
cp -p -f miscTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/miscTypes.h
cp -p -f tecplotUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/tecplotUtils.h
cp -p -f vlmSpanSpace.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/vlmSpanSpace.h
cp -p -f cardUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cardUtils.h
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/utils'
make -C friction 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/friction'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -Wno-format -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils frictionAIM.c \
	-o ./frictionAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/frictionAIM.so ./frictionAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer friction_eja_mod.f -o ./friction.o
gfortran -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/friction ./friction.o 
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/friction'
make -C tetgen 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tetgen'
g++ -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils tetgenAIM.cpp \
	-o ./tetgenAIM.o
g++ -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I/home/jenkins/util/tetgen/tetgen1.6.0 -I../utils \
	-DTETLIBRARY tetgen_Interface.cpp -o ./tetgen_Interface.o
g++ -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DTETLIBRARY -w /home/jenkins/util/tetgen/tetgen1.6.0/tetgen.cxx -o ./tetgen.o
g++ -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -O0 -w /home/jenkins/util/tetgen/tetgen1.6.0/predicates.cxx -o ./predicates.o
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tetgenAIM.so ./tetgenAIM.o \
	./tetgen_Interface.o ./tetgen.o \
	./predicates.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \
	-legads -ludunits2 -ldl -lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tetgen'
make -C tacs 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tacs'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils tacsAIM.c \
	-o ./tacsAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tacsAIM.so ./tacsAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tacs'
make -C astros 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/astros'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils astrosAIM.c \
	-o ./astrosAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils astrosUtils.c \
	-o ./astrosUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils astrosCards.c \
        -o ./astrosCards.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/astrosAIM.so ./astrosAIM.o  ./astrosUtils.o ./astrosCards.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/astros'
make -C pointwise 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/pointwise'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils pointwiseAIM.c \
	-o ./pointwiseAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils hashElement.c \
	-o ./hashElement.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pointwiseAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pointwiseAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pointwiseAIM.so ./pointwiseAIM.o ./hashElement.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
	-lrt -lm -lpthread
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/pointwise'
make -C xfoil 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/xfoil'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
	xfoilAIM.c -o ./xfoilAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/xfoilAIM.so ./xfoilAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/xfoil'
make -C aflr2 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr2'
Not compiling aflr2AIM: AFLR must be set -- Please fix the environment....
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr2'
make -C aflr4 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr4'
Not compiling aflr4AIM: AFLR must be set -- Please fix the environment....
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr4'
make -C su2 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/su2'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../meshWriter/su2Writer -I../utils su2AIM.c \
	-o ./su2AIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2Utils.c \
	-o ./su2Utils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_4_Cardinal.c \
	-o ./su2_4_Cardinal.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_5_Raven.c \
	-o ./su2_5_Raven.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_6_Falcon.c \
	-o ./su2_6_Falcon.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_7_Blackbird.c \
	-o ./su2_7_Blackbird.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_801_Harrier.c \
	-o ./su2_801_Harrier.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/su2AIM.so ./su2AIM.o ./su2Utils.o ./su2_4_Cardinal.o ./su2_5_Raven.o ./su2_6_Falcon.o ./su2_7_Blackbird.o ./su2_801_Harrier.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/su2'
make -C cgt 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cgt'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include egads2cgt.c \
	-o ./egads2cgt.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include aflr4egads.c \
	-o ./aflr4egads.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/egads2cgt ./egads2cgt.o ./aflr4egads.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads -lcaps -locsm -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cgt'
make -C mses 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/mses'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils msesAIM.c -o msesAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils msesUtils.c -o msesUtils.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/msesAIM.so ./msesAIM.o ./msesUtils.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/mses'
make -C egadsTess 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/egadsTess'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils egadsTessAIM.c \
	-o ./egadsTessAIM.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/egadsTessAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/egadsTessAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/egadsTessAIM.so ./egadsTessAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
	-lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/egadsTess'
make -C sierraSD 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/sierraSD'
Not compiling sierraSDAIM: SEACAS must be set -- Please fix the environment....
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/sierraSD'
make -C masstran 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/masstran'
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils masstranAIM.cpp \
	-o ./masstranAIM.o
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/masstranAIM.so ./masstranAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/masstran'
make -C plato 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/plato'
Not compiling platoAIM: SEACAS must be set -- Please fix the environment....
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/plato'
make -C refine 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/refine'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/libmeshbWriter refineAIM.c \
	-o ./refineAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 \
	-I../meshWriter/libmeshbWriter/libMeshb/sources \
	../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \
	-o ./libmeshb7.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/refineAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/refineAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/refineAIM.so ./refineAIM.o ./libmeshb7.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
	-lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/refine'
make -C awave 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/awave'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils awaveAIM.c \
	-o ./awaveAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/awaveAIM.so ./awaveAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/awave'
make -C tsfoil 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tsfoil'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
	tsfoilAIM.c -o ./tsfoilAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tsfoilAIM.so ./tsfoilAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tsfoil'
make -C delaundo 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/delaundo'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils delaundoAIM.c \
	-o ./delaundoAIM.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/delaundoAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/delaundoAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/delaundoAIM.so ./delaundoAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
	-lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/delaundo'
make -C abaqus 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/abaqus'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
	abaqusAIM.c -o ./abaqusAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
	abaqusUtils.c -o ./abaqusUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
	-I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/abaqusFILReader.c -o ./abaqusFILReader.o
echo "Building Abaqus with Python"
Building Abaqus with Python
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/abaqusAIM.so ./abaqusAIM.o ./abaqusUtils.o ./abaqusFILReader.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lm -ldl -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/abaqus'
make -C fun3d 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/fun3d'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
	-I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \
	-I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython fun3dAIM.c -o ./fun3dAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \
	fun3dUtils.c -o ./fun3dUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
	-I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
	-I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/fun3dNamelist.c -o ./fun3dNamelist.o
Building FUN3D with Python
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fun3dAIM.so ./fun3dAIM.o ./fun3dUtils.o \
	./fun3dNamelist.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \
	-legads -ludunits2 -ldl -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lm -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/fun3d'
make -C cbaero 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cbaero'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o cbaeroAIM.o
gcc -g  -shared -Wl,-no-undefined  cbaeroAIM.o -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/cbaeroAIM.so -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cbaero'
make -C interference 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/interference'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include interferenceAIM.c \
	-o ./interferenceAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. cloudFns.c \
	-o ./cloudFns.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/interferenceAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/interferenceAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/interferenceAIM.so \
	./interferenceAIM.o ./cloudFns.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib \
	-laimUtil -locsm -legads -ludunits2 -ldl -lstdc++ -lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/interference'
make -C meshWriter 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter'
make -C libmeshbWriter 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/libmeshbWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include libmeshbWriter.c \
	-o ./libmeshbWriter.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -IlibMeshb/sources -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include libMeshb/sources/libmeshb7.c \
	-o ./libmeshb7.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libmeshbWriter.so ./libmeshbWriter.o ./libmeshb7.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/libmeshbWriter'
make -C fastWriter 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/fastWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include fastWriter.c \
	-o ./fastWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fastWriter.so ./fastWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/fastWriter'
make -C tecplotWriter 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/tecplotWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include tecplotWriter.c \
	-o ./tecplotWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tecplotWriter.so ./tecplotWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/tecplotWriter'
make -C vtkWriter 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/vtkWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include vtkWriter.c \
	-o ./vtkWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vtkWriter.so ./vtkWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/vtkWriter'
make -C bstlWriter 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bstlWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include bstlWriter.c \
	-o ./bstlWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bstlWriter.so ./bstlWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bstlWriter'
make -C bvtkWriter 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bvtkWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include bvtkWriter.c \
	-o ./bvtkWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bvtkWriter.so ./bvtkWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bvtkWriter'
make -C su2Writer 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/su2Writer'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include su2Writer.c \
	-o ./su2Writer.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/su2Writer.so ./su2Writer.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/su2Writer'
make -C stlWriter 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/stlWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include stlWriter.c \
	-o ./stlWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stlWriter.so ./stlWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/stlWriter'
make -C ugridWriter 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/ugridWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include ugridWriter.c \
	-o ./ugridWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ugridWriter.so ./ugridWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/ugridWriter'
make -C exodusWriter 
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/exodusWriter'
make[3]: Nothing to be done for 'default'.
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/exodusWriter'
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter'
make -C cart3d 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cart3d'
make -C nastran 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/nastran'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils nastranAIM.c \
	-o ./nastranAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nastranAIM.so ./nastranAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/nastran'
make -C spinnaker 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/spinnaker'
make[2]: Nothing to be done for 'default'.
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/spinnaker'
make -C aflr3 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr3'
Not compiling aflr3AIM: AFLR must be set -- Please fix the environment....
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr3'
make -C sierraSM 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/sierraSM'
Not compiling sierraSMAIM: SEACAS must be set -- Please fix the environment....
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/sierraSM'
make -C hsm 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils hsmAIM.c \
	-o src/hsmAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils hsmUtils.c \
	-o src/hsmUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils hsmAdj.c \
	-o src/hsmAdj.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -Wno-comment rcm/rcm.cpp -DREVISION=7.8 \
	-o src/rcm.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 rcm/genrcmi.cpp -DREVISION=7.8 \
	-o src/genrcmi.o
make -C src hsmglr.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmglr.f -o ./hsmglr.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmbc.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmbc.f -o ./hsmbc.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmbb2.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmbb2.f -o ./hsmbb2.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmre1.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmre1.f -o ./hsmre1.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmdep.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmdep.f -o ./hsmdep.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmrfm.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmrfm.f -o ./hsmrfm.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmout.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmout.f -o ./hsmout.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmren.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmren.f -o ./hsmren.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmprj.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmprj.f -o ./hsmprj.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src atanc.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  atanc.f -o ./atanc.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src cross.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  cross.f -o ./cross.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src ludcmp.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  ludcmp.f -o ./ludcmp.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmabd.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmabd.f -o ./hsmabd.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src bmdump.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  bmdump.f -o ./bmdump.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmrun.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero -fno-recursive hsmrun.f -o ./hsmrun.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmeqn.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmeqn.f -o ./hsmeqn.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmsol.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmsol.f -o ./hsmsol.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmgeo.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmgeo.f -o ./hsmgeo.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src sbsolve.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  sbsolve.f -o ./sbsolve.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a hsmsol.o hsmdep.o hsmout.o hsmgeo.o hsmabd.o hsmeqn.o hsmbc.o hsmprj.o hsmren.o hsmre1.o hsmrfm.o hsmbb2.o hsmglr.o ludcmp.o sbsolve.o atanc.o bmdump.o cross.o )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hsmAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hsmAIM.so
gfortran -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hsmAIM.so \
	src/hsmAIM.o src/hsmUtils.o src/hsmAdj.o \
	src/rcm.o src/genrcmi.o \
	 -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \
	-legads -ludunits2 -lhsm -ldl  -lstdc++ 
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm'
make -C avl 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/avl'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils avlAIM.c -o ./avlAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o avlRead_ELE.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o avlRead_DERMATB.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o avlRead_HINGE.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o avlRead_BODY.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o avlRead_CNC.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o avlRead_TOT.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o avlRead_DERMATS.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o avlRead_STRP.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o avlRead_VM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o avlRead_CPOML.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o avlRead_DERMATM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o avlRead_SURF.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/avlAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/avlAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/avlAIM.so ./avlAIM.o ./avlRead_ELE.o ./avlRead_DERMATB.o ./avlRead_HINGE.o ./avlRead_BODY.o ./avlRead_CNC.o ./avlRead_TOT.o ./avlRead_DERMATS.o ./avlRead_STRP.o ./avlRead_VM.o ./avlRead_CPOML.o ./avlRead_DERMATM.o ./avlRead_SURF.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \
	-lstdc++ -lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/avl'
make -C custom 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/custom'
make[2]: Nothing to be done for 'default'.
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/custom'
make -C skeleton 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/skeleton'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils skeletonAIM.c \
	-o ./skeletonAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/skeletonAIM.so ./skeletonAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/skeleton'
make -C unitTest 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest'
make[2]: Nothing to be done for 'all'.
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest'
make -C mystran 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/mystran'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils mystranAIM.c \
	-o ./mystranAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils mystranUtils.c \
	-o ./mystranUtils.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mystranAIM.so ./mystranAIM.o ./mystranUtils.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/mystran'
make -C zaero 
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/zaero'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroAIM.c -o zaeroAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroUtils.c -o zaeroUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroLinearFlutter.c -o zaeroLinearFlutter.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroTrim.c -o zaeroTrim.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroTypes.c -o zaeroTypes.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroCards.c -o zaeroCards.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroGeneral.c -o zaeroGeneral.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroGraphical.c -o zaeroGraphical.o
gcc -g  -shared -Wl,-no-undefined   -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/zaeroAIM.so ./zaeroAIM.o ./zaeroUtils.o ./zaeroLinearFlutter.o ./zaeroTrim.o ./zaeroTypes.o ./zaeroCards.o ./zaeroGeneral.o ./zaeroGraphical.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/zaero'
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim'
(cd OpenCSM; make -f serveESP.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/OpenCSM'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timCapsMode.c -o ./timCapsMode.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/capsMode.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/capsMode.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/capsMode.so ./timCapsMode.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timFlowchart.c -o ./timFlowchart.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flowchart.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flowchart.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flowchart.so ./timFlowchart.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timViewer.c -o ./timViewer.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/viewer.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/viewer.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/viewer.so ./timViewer.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 timPyscript.c -o ./timPyscript.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pyscript.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pyscript.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pyscript.so ./timPyscript.o -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lrt -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/OpenCSM'
 
 *** Build Completed! ***
+ export CSMDATA=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data
+ CSMDATA=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin
++ uname -a
+ [[ Linux reynolds-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/7.8/LINUX64/Verification.sh
+ bash -ex /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/Verification.sh
+ expectSuccess 01 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/expressions.vfy", so verification is being skipped
ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set)
ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set)
ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set)
==> serveESP completed successfully with no verification data

real	0m0.134s
user	0m0.080s
sys	0m0.019s
+ set +x

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

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

real	0m0.310s
user	0m0.377s
sys	0m0.021s
+ set +x

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

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

real	0m2.628s
user	0m3.711s
sys	0m0.108s
+ set +x

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

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

real	0m0.533s
user	0m0.776s
sys	0m0.024s
+ set +x

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

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

real	0m0.567s
user	0m0.829s
sys	0m0.025s
+ set +x

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

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

real	0m0.386s
user	0m0.760s
sys	0m0.016s
+ set +x

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

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

real	0m3.742s
user	0m5.817s
sys	0m0.068s
+ set +x

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

+ expectSuccess 08 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/CAPS/myPlane
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/CAPS/myPlane
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/CAPS/verify_7.8.0/myPlane.vfy", so verification is being skipped
==> serveESP completed successfully with 12 warnings and no verification data

real	0m27.346s
user	0m44.900s
sys	0m0.368s
+ set +x

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

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

real	0m0.543s
user	0m0.770s
sys	0m0.022s
+ set +x

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

+ expectSuccess 10 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/wingMultiModel
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/wingMultiModel
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/wingMultiModel.vfy", so verification is being skipped
==> serveESP completed successfully with 4 warnings and no verification data

real	0m33.668s
user	1m1.344s
sys	0m1.603s
+ set +x

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

+ expectSuccess 11 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/bullet
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/bullet
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/bullet.vfy", so verification is being skipped
WARNING:: 8 _hist and/or __trace__ attributes removed
WARNING:: 8 _hist and/or __trace__ attributes removed
WARNING:: could not find mapping for iedge=10
WARNING:: could not find mapping for iedge=14
WARNING:: could not find mapping for iedge=7
WARNING:: could not find mapping for iedge=11
==> serveESP completed successfully with 5 warnings and no verification data

real	0m0.321s
user	0m0.350s
sys	0m0.021s
+ set +x

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

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

real	0m0.506s
user	0m0.812s
sys	0m0.020s
+ set +x

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

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

real	0m0.175s
user	0m0.199s
sys	0m0.021s
+ set +x

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

+ expectSuccess 14 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/csm3
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/csm3
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/csm3.vfy", so verification is being skipped
nnode=8
nedge=12
nface=6
nnode=8
nedge=12
nface=6
nnode=16
nedge=24
nface=10
nnode=8
nedge=12
nface=6
==> serveESP completed successfully with no verification data

real	0m0.422s
user	0m0.591s
sys	0m0.030s
+ set +x

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

+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/testEGADS
+ make test
python --version
Python 3.11.9
python -u -m unittest discover
....................................................   PCurve Map: 48 (alloc 48)!
   Surface Map: 12 (alloc 24)!
   Curve Map: 28 (alloc 28)!
 Writing PCurves...
 Writing Curves...
 Writing Surfaces...
 Writing 16 Nodes...
 Writing 28 Edges...
 Writing 12 Loops...
 Writing 12 Faces...
 Writing 1 Shells...
 EGADS Info: 0 Objects, 0 Reference in Use (of 972) at Close!
...................
----------------------------------------------------------------------
Ran 71 tests in 2.303s

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

real	0m5.877s
user	0m9.914s
sys	0m0.144s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/testCAPS
+ make test
python --version
Python 3.11.9
python -u -m unittest discover
..Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

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

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

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

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

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

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

----------------------------------------------------------------------
Ran 100 tests in 13.679s

OK
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/
+ make test
python --version
Python 3.11.9
python -u -m unittest discover --verbose
Please set the environment variable ASTROS_ROOT
test_journal (test_aflr2.TestAFLR2.test_journal) ... Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2    : Compile Date   04/23/24 @ 12:17PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2244         0
 
AFLR2    : CPU Time          =     0.001   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          =     0.127   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.011   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
Getting 2D mesh for body 1 (of 1)
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2224         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2224      2224
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       446       894
AFLR2 IG : Nodes, Faces      =       892      1786
AFLR2 IG : Nodes, Faces      =       918      1838
AFLR2 IG : Nodes, Faces      =      1033      2068
AFLR2 IG : Nodes, Faces      =      1133      2268
AFLR2 IG : Nodes, Faces      =      1233      2468
AFLR2 IG : Nodes, Faces      =      1333      2668
AFLR2 IG : Nodes, Faces      =      1338      2678
AFLR2 IG : Nodes, Faces      =      1433      2868
AFLR2 IG : Nodes, Faces      =      1533      3068
AFLR2 IG : Nodes, Faces      =      1633      3268
AFLR2 IG : Nodes, Faces      =      1733      3468
AFLR2 IG : Nodes, Faces      =      1784      3570
AFLR2 IG : Nodes, Faces      =      1833      3668
AFLR2 IG : Nodes, Faces      =      1858      3718
AFLR2 IG : Nodes, Faces      =      2224      4450
AFLR2 IG : Nodes, Faces      =      2228      4450
AFLR2 IG : Nodes, Faces      =      2224      2224
 
AFLR2    : CPU Time          =     0.033   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          =     0.116   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     23187     44150
 
AFLR2    : CPU Time          =     0.009   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          =     0.041   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          =     0.097   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.008   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
 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          =     0.001   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          =     0.071   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          =     0.124   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     23187     44150
 
AFLR2    : CPU Time          =     0.038   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          =     0.072   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          =     0.131   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.010   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          =     0.009   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      4705      9066
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

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

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


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

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


Writing vtk file ....

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


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


Writing FAST file ....
Finished writing FAST file


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


Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       339       680
AFLR2 IG : Nodes, Faces      =       340       682
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       682      1020
AFLR2 GGp: Nodes, Faces      =      1010      1676
AFLR2 GGp: Nodes, Faces      =      1316      2288
AFLR2 GGp: Nodes, Faces      =      1592      2840
AFLR2 GGp: Nodes, Faces      =      1855      3366
AFLR2 GGp: Nodes, Faces      =      2106      3868
AFLR2 GGp: Nodes, Faces      =      2341      4338
AFLR2 GGp: Nodes, Faces      =      2551      4758
AFLR2 GGp: Nodes, Faces      =      2741      5138
AFLR2 GGp: Nodes, Faces      =      2917      5490
AFLR2 GGp: Nodes, Faces      =      3082      5820
AFLR2 GGp: Nodes, Faces      =      3240      6136
AFLR2 GGp: Nodes, Faces      =      3379      6414
AFLR2 GGp: Nodes, Faces      =      3513      6682
AFLR2 GGp: Nodes, Faces      =      3642      6940
AFLR2 GGp: Nodes, Faces      =      3748      7152
AFLR2 GGp: Nodes, Faces      =      3846      7348
AFLR2 GGp: Nodes, Faces      =      3931      7518
AFLR2 GGp: Nodes, Faces      =      3999      7654
AFLR2 GGp: Nodes, Faces      =      4044      7744
AFLR2 GGp: Nodes, Faces      =      4058      7772
 
AFLR2    : CPU Time          =     0.012   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 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          =     0.008   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 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:62511)
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 7):
	Number of nodes          = 1189
	Number of elements       = 6249
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4917
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cylinder, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 7 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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:62511)
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2589
	Number of elements       = 13809
	Number of triangles      = 2758
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 11051
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 4694
	Number of elements       = 25935
	Number of triangles      = 3326
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 22609
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5554
	Number of elements       = 30862
	Number of triangles      = 3756
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 27106
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2260
	Number of elements       = 12133
	Number of triangles      = 2222
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 9911
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2392
	Number of elements       = 12577
	Number of triangles      = 2666
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 9911
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 2):
	Number of nodes          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 2):
	Number of nodes          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 3341
	Number of elements       = 18069
	Number of triangles      = 3110
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 14959
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 3606
	Number of elements       = 18961
	Number of triangles      = 4002
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 14959
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 4414
	Number of elements       = 23974
	Number of triangles      = 3998
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 19976
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 4)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 4)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 4)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 4811
	Number of elements       = 25310
	Number of triangles      = 5334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 19976
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 4):
	Number of nodes          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 4):
	Number of nodes          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 4):
	Number of nodes          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 4):
	Number of nodes          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5490
	Number of elements       = 29891
	Number of triangles      = 4886
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 25005
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 6019
	Number of elements       = 31671
	Number of triangles      = 6666
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 25005
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 5):
	Number of nodes          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 5):
	Number of nodes          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 5):
	Number of nodes          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 5):
	Number of nodes          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 5):
	Number of nodes          = 1208
	Number of elements       = 6361
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5029
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 6542
	Number of elements       = 35667
	Number of triangles      = 5774
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 29893
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 7203
	Number of elements       = 37891
	Number of triangles      = 7998
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 29893
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 6):
	Number of nodes          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 6):
	Number of nodes          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 6):
	Number of nodes          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 6):
	Number of nodes          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 6):
	Number of nodes          = 1208
	Number of elements       = 6361
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5029
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 6 (of 6):
	Number of nodes          = 1184
	Number of elements       = 6220
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4888
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 7601
	Number of elements       = 41489
	Number of triangles      = 6662
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 34827
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 7 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 8394
	Number of elements       = 44157
	Number of triangles      = 9330
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 34827
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 7):
	Number of nodes          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 7):
	Number of nodes          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 7):
	Number of nodes          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 7):
	Number of nodes          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 7):
	Number of nodes          = 1208
	Number of elements       = 6361
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5029
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 6 (of 7):
	Number of nodes          = 1184
	Number of elements       = 6220
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4888
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 7 (of 7):
	Number of nodes          = 1191
	Number of elements       = 6266
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4934
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 19800
	Number of elements       = 109798
	Number of triangles      = 15540
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 94258
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 7 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 8 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 9 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 10 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 11 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 12 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 13 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 14 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 15 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 16 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 17 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 18 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 19 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 22741
	Number of elements       = 119570
	Number of triangles      = 25312
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 94258
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 19):
	Number of nodes          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 19):
	Number of nodes          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 19):
	Number of nodes          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 19):
	Number of nodes          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 19):
	Number of nodes          = 1208
	Number of elements       = 6361
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5029
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 6 (of 19):
	Number of nodes          = 1184
	Number of elements       = 6220
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4888
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 7 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 7 (of 19):
	Number of nodes          = 1191
	Number of elements       = 6266
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4934
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 8 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 8 (of 19):
	Number of nodes          = 1193
	Number of elements       = 6272
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4940
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 9 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 9 (of 19):
	Number of nodes          = 1176
	Number of elements       = 6165
	Number of triangles      = 1330
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4835
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 10 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 10 (of 19):
	Number of nodes          = 1203
	Number of elements       = 6314
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4982
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 11 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 11 (of 19):
	Number of nodes          = 1192
	Number of elements       = 6269
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4937
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 12 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 12 (of 19):
	Number of nodes          = 1192
	Number of elements       = 6269
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4937
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 13 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 13 (of 19):
	Number of nodes          = 1198
	Number of elements       = 6296
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4964
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 14 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 14 (of 19):
	Number of nodes          = 1223
	Number of elements       = 6443
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5111
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 15 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 15 (of 19):
	Number of nodes          = 1184
	Number of elements       = 6224
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4892
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 16 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 16 (of 19):
	Number of nodes          = 1195
	Number of elements       = 6287
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4955
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 17 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 17 (of 19):
	Number of nodes          = 1197
	Number of elements       = 6311
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4979
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 18 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 18 (of 19):
	Number of nodes          = 1203
	Number of elements       = 6310
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4978
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 19 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 19 (of 19):
	Number of nodes          = 1191
	Number of elements       = 6253
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4921
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 8857
	Number of elements       = 49191
	Number of triangles      = 6284
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 42907
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 8989
	Number of elements       = 49635
	Number of triangles      = 6728
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 42907
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 2):
	Number of nodes          = 7796
	Number of elements       = 43368
	Number of triangles      = 5396
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 37972
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 2):
	Number of nodes          = 1193
	Number of elements       = 6267
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4935
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9944
	Number of elements       = 55193
	Number of triangles      = 7174
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 48019
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 10218
	Number of elements       = 56081
	Number of triangles      = 8062
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 48019
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7818
	Number of elements       = 43469
	Number of triangles      = 5398
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 38071
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 1202
	Number of elements       = 6320
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4988
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 1198
	Number of elements       = 6292
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4960
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9609
	Number of elements       = 53228
	Number of triangles      = 6994
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 46234
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9829
	Number of elements       = 53956
	Number of triangles      = 7722
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 46234
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7789
	Number of elements       = 43295
	Number of triangles      = 5394
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 37901
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 1186
	Number of elements       = 6230
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4898
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 854
	Number of elements       = 4431
	Number of triangles      = 996
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 3435
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9348
	Number of elements       = 51734
	Number of triangles      = 6812
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44922
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9531
	Number of elements       = 52330
	Number of triangles      = 7408
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44922
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7804
	Number of elements       = 43358
	Number of triangles      = 5386
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 37972
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 1200
	Number of elements       = 6311
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4979
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 527
	Number of elements       = 2661
	Number of triangles      = 690
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1971
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9183
	Number of elements       = 50871
	Number of triangles      = 6632
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44239
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9322
	Number of elements       = 51307
	Number of triangles      = 7068
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44239
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7927
	Number of elements       = 44116
	Number of triangles      = 5382
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 38734
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 868
	Number of elements       = 4530
	Number of triangles      = 996
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 3534
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 527
	Number of elements       = 2661
	Number of triangles      = 690
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1971
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 10181
	Number of elements       = 56797
	Number of triangles      = 6782
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 50015
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 10671
	Number of elements       = 58561
	Number of triangles      = 8546
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 50015
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7741
	Number of elements       = 43010
	Number of triangles      = 5362
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 37648
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 2692
	Number of elements       = 14435
	Number of triangles      = 2800
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 11635
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 238
	Number of elements       = 1116
	Number of triangles      = 384
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 732
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 1500
	Number of elements       = 7757
	Number of triangles      = 1986
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5771
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 1564
	Number of elements       = 7881
	Number of triangles      = 2110
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5771
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 1160
	Number of elements       = 6087
	Number of triangles      = 1308
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4779
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 360
	Number of elements       = 1635
	Number of triangles      = 718
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 917
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 44
	Number of elements       = 159
	Number of triangles      = 84
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 75
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 2):
	Number of nodes          = 336
	Number of elements       = 1507
	Number of triangles      = 584
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 923
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 5):
	Number of nodes          = 1415
	Number of elements       = 7515
	Number of triangles      = 1456
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6059
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 5):
	Number of nodes          = 711
	Number of elements       = 3685
	Number of triangles      = 844
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 2841
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 5):
	Number of nodes          = 1253
	Number of elements       = 6578
	Number of triangles      = 1424
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5154
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2940
	Number of elements       = 12771
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7319
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2497
	Number of elements       = 10947
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6395
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2940
	Number of elements       = 12771
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7319
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2497
	Number of elements       = 10947
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6395
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
ok
test_phase (test_aflr3.TestAFLR3.test_phase) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2940
	Number of elements       = 12771
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7319
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2497
	Number of elements       = 10947
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6395
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2940
	Number of elements       = 12771
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7319
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

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


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


Writing Tecplot file ....
Finished writing Tecplot file


Writing vtk file ....

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


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


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file

Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2497
	Number of elements       = 10947
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6395
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

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


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


Writing Tecplot file ....
Finished writing Tecplot file


Writing vtk file ....

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


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


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5047
	Number of elements       = 27987
	Number of triangles      = 3464
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 24523
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
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:62511)
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:62511)
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:62511)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
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:62511)
 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:62511)
 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:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 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:62511)
 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:62511)
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
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:62511)
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_regions (test_aflr4.TestAFLR4.test_regions) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

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: box
  2: cut
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_structures (test_aflr4.TestAFLR4.test_structures) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2

Writing 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: Ribs
  2: Skin
  3: Spar1
  4: Rib_Root
  5: Spar2
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_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_v5 (test_cbaero.TestCBAERO.test_Output_v5) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = Wing1, index = 1
	Name = trailingEdge, index = 2

Writing FAST file ....
Finished writing FAST file

Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_Output_v6 (test_cbaero.TestCBAERO.test_Output_v6) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_inputs (test_cbaero.TestCBAERO.test_inputs) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_MultiBody (test_egadsTess.TestEGADS.test_MultiBody) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4

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

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
ok
test_all (test_egadsTess.TestEGADS.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
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
 7F0B3B384700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F0B3B384700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7F0B5D59B740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F0B5D59B740 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
 7F0B3B384700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F0B3B384700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7F0B40FB1700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F0B40FB1700 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
 7F0B5D59B740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F0B5D59B740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7F0B3B384700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F0B3B384700 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
 7F0B5D59B740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F0B5D59B740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7F0B417B2700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F0B417B2700 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:62511)
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:62511)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
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:62511)
 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:62511)
 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:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 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:62511)
 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:62511)
 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:62511)
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:62511)
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:62511)
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:  0.165465
Creating surface mesh ...
Surface mesh seconds:  0.043559
Recovering boundaries...
Boundary recovery seconds:  0.200653
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.087228
Recovering Delaunayness...
Delaunay recovery seconds:  0.084287
Refining mesh...
  18827 insertions, added 13420 points, 721721 tetrahedra in queue.
  6269 insertions, added 2485 points, 625204 tetrahedra in queue.
  8356 insertions, added 2101 points, 168215 tetrahedra in queue.
Refinement seconds:  3.49535
Smoothing vertices...
Mesh smoothing seconds:  3.18288
Improving mesh...
Mesh improvement seconds:  0.063483

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

Output seconds:  0.020315
Total running seconds:  7.34394

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:  0.165984
Creating surface mesh ...
Surface mesh seconds:  0.043813
Recovering boundaries...
Boundary recovery seconds:  0.200473
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.087088
Recovering Delaunayness...
Delaunay recovery seconds:  0.08434
Refining mesh...
  18827 insertions, added 13420 points, 721721 tetrahedra in queue.
  6269 insertions, added 2485 points, 625204 tetrahedra in queue.
  8356 insertions, added 2101 points, 168215 tetrahedra in queue.
Refinement seconds:  3.3866
Smoothing vertices...
Mesh smoothing seconds:  3.23788
Improving mesh...
Mesh improvement seconds:  0.064008

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

Output seconds:  0.020673
Total running seconds:  7.29157

Statistics:

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

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

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

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)

	Reading /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM4/fun3d.nml .....
	Appending namelist
	Done writing nml file with Python
Info: No recognized data transfer names found.
ok
test_cythonNMLError (test_fun3d.TestFUN3D.test_cythonNMLError) ... ok
test_cythonNMLReentrance (test_fun3d.TestFUN3D.test_cythonNMLReentrance) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)
	/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml not found!
	Creating namelist
	Done writing nml file with Python
Info: No recognized data transfer names found.

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)

	Reading /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml .....
	Appending namelist
	Done writing nml file with Python
Info: No recognized data transfer names found.
ok
test_invalidBoundary (test_fun3d.TestFUN3D.test_invalidBoundary) ... Getting CFD boundary conditions
	Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_fun3d.TestFUN3D.test_invalidBoundaryName) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - X
ok
test_journal (test_fun3d.TestFUN3D.test_journal) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 5043, elements - 10074
Getting volume mesh

Generating volume mesh using TetGen.....

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

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

Writing MAPBC file ....
Finished writing MAPBC file

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

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 5043, elements - 10074
Getting volume mesh

Generating volume mesh using TetGen.....

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

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

Writing MAPBC file ....
Finished writing MAPBC file

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

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

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

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

Writing MAPBC file ....
Finished writing MAPBC file

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

Writing MAPBC file ....
Finished writing MAPBC file

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

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 14124, elements - 28236
Getting volume mesh

Generating volume mesh using TetGen.....

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

Writing MAPBC file ....
Finished writing MAPBC file

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

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

Writing MAPBC file ....
Finished writing MAPBC file

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

Writing MAPBC file ....
Finished writing MAPBC file

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

Writing MAPBC file ....
Finished writing MAPBC file

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

Writing MAPBC file ....
Finished writing MAPBC file

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
ok
test_MultiBody (test_pointwise.TestPointwise.test_MultiBody) ... skipped 'No pointwise executable'
test_SingleBody (test_pointwise.TestPointwise.test_SingleBody) ... skipped 'No pointwise executable'
test_all (test_pointwise.TestPointwise.test_all) ... skipped 'No pointwise executable'
test_box (test_pointwise.TestPointwise.test_box) ... skipped 'No pointwise executable'
test_bullet (test_pointwise.TestPointwise.test_bullet) ... skipped 'No pointwise executable'
test_cone (test_pointwise.TestPointwise.test_cone) ... skipped 'No pointwise executable'
test_cylinder (test_pointwise.TestPointwise.test_cylinder) ... skipped 'No pointwise executable'
test_executeError (test_pointwise.TestPointwise.test_executeError) ... skipped 'No pointwise executable'
test_reenter (test_pointwise.TestPointwise.test_reenter) ... skipped 'No pointwise executable'
test_sphere (test_pointwise.TestPointwise.test_sphere) ... skipped 'No pointwise executable'
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
test_Area_Mesh (test_refine.TestREFINE.test_Area_Mesh) ... skipped "No 'ref' executable"
test_all (test_refine.TestREFINE.test_all) ... skipped "No 'ref' executable"
test_box_volume (test_refine.TestREFINE.test_box_volume) ... skipped "No 'ref' executable"
test_boxhole (test_refine.TestREFINE.test_boxhole) ... skipped "No 'ref' executable"
test_cfdSingleBody (test_refine.TestREFINE.test_cfdSingleBody) ... skipped "No 'ref' executable"
test_fun3d (test_refine.TestREFINE.test_fun3d) ... skipped "No 'ref' executable"
test_inputs (test_refine.TestREFINE.test_inputs) ... skipped "No 'ref' executable"
test_phase (test_refine.TestREFINE.test_phase) ... skipped "No 'ref' executable"
test_sphere (test_refine.TestREFINE.test_sphere) ... skipped "No 'ref' executable"
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
test_inputs (test_su2.TestSU2.test_inputs) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting volume mesh
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mpfrmt                      = 0         

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 3 Active Bodies

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

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

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

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

EGADS    : Face Edges Information

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

EGADS    : Face Loops Information

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

EGADS    : Loop Edges Information

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

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

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

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

EGADS    : Node Information

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

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

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

AFLR4    : Geometry Definition Information

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

AFLR4    : Case has 2 Proximity Checking Components

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

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

UG3      : Boundary Conditions

UG3      :  B-Face ID            Boundary Condition
UG3      :          1                         Solid
UG3      :          2                         Solid
UG3      :          3                         Solid
UG3      :          4                         Solid
UG3      :          5                         Solid
UG3      :          6                         Solid
UG3      :          7                         Solid
UG3      :          8                         Solid
UG3      :          9                         Solid
UG3      :         10                         Solid
UG3      :         11                         Solid
UG3      :         12                         Solid
UG3      :         13                         Solid
UG3      :         14                         Solid
UG3      :         15                         Solid
UG3      :         16                         Solid
UG3      :         17                      FarField
UG3      :         18                      FarField
 
AFLR3    : CPU Time          =     0.020   seconds
 
AFLR3 IG : INITIAL VOLUME GRID GENERATION
 
AFLR3 IG : Nodes, Elements   =      6220         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =      1246      7333
AFLR3 IG : Nodes, Elements   =      2492     16261
AFLR3 IG : Nodes, Elements   =      3738     25021
AFLR3 IG : Nodes, Elements   =      4984     34304
AFLR3 IG : Nodes, Elements   =      6227     43518
AFLR3 IG : Nodes, Elements   =      6227     43440
AFLR3 IG : Nodes, Elements   =      6227     43475
AFLR3 IG : Nodes, Elements   =      6227     43439
AFLR3 IG : Nodes, Elements   =      6220     26110
AFLR3 IG : Nodes, Elements   =      6220     26133
AFLR3 IG : Nodes, Elements   =      6220     21491
AFLR3 IG : Nodes, Elements   =      6220     19188
 
AFLR3    : CPU Time          =     0.270   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =      6220     19188
AFLR3 GG : Nodes, Elements   =      9098     28027
AFLR3 GG : Nodes, Elements   =      9098     39406
AFLR3 GG : Nodes, Elements   =      9098     36704
AFLR3 GG : Nodes, Elements   =      9098     35224
AFLR3 GG : Nodes, Elements   =     11628     43169
AFLR3 GG : Nodes, Elements   =     11628     53705
AFLR3 GG : Nodes, Elements   =     11628     50685
AFLR3 GG : Nodes, Elements   =     11628     49794
AFLR3 GG : Nodes, Elements   =     14415     58408
AFLR3 GG : Nodes, Elements   =     14415     70501
AFLR3 GG : Nodes, Elements   =     14415     67147
AFLR3 GG : Nodes, Elements   =     14415     66320
AFLR3 GG : Nodes, Elements   =     17361     75337
AFLR3 GG : Nodes, Elements   =     17361     88116
AFLR3 GG : Nodes, Elements   =     17361     84624
AFLR3 GG : Nodes, Elements   =     17361     83829
AFLR3 GG : Nodes, Elements   =     20551     93587
AFLR3 GG : Nodes, Elements   =     20551    107171
AFLR3 GG : Nodes, Elements   =     20551    103485
AFLR3 GG : Nodes, Elements   =     20551    102651
AFLR3 GG : Nodes, Elements   =     23820    112676
AFLR3 GG : Nodes, Elements   =     23820    126717
AFLR3 GG : Nodes, Elements   =     23820    122888
AFLR3 GG : Nodes, Elements   =     23820    122008
AFLR3 GG : Nodes, Elements   =     27245    132431
AFLR3 GG : Nodes, Elements   =     27245    147117
AFLR3 GG : Nodes, Elements   =     27245    143166
AFLR3 GG : Nodes, Elements   =     27245    142222
AFLR3 GG : Nodes, Elements   =     30783    152976
AFLR3 GG : Nodes, Elements   =     30783    168143
AFLR3 GG : Nodes, Elements   =     30783    164070
AFLR3 GG : Nodes, Elements   =     30783    163175
AFLR3 GG : Nodes, Elements   =     34292    173827
AFLR3 GG : Nodes, Elements   =     34292    188808
AFLR3 GG : Nodes, Elements   =     34292    184786
AFLR3 GG : Nodes, Elements   =     34292    183954
AFLR3 GG : Nodes, Elements   =     37874    194791
AFLR3 GG : Nodes, Elements   =     37874    210042
AFLR3 GG : Nodes, Elements   =     37874    206016
AFLR3 GG : Nodes, Elements   =     37874    205187
AFLR3 GG : Nodes, Elements   =     41380    215779
AFLR3 GG : Nodes, Elements   =     41380    230857
AFLR3 GG : Nodes, Elements   =     41380    226861
AFLR3 GG : Nodes, Elements   =     41380    226096
AFLR3 GG : Nodes, Elements   =     44867    236615
AFLR3 GG : Nodes, Elements   =     44867    251351
AFLR3 GG : Nodes, Elements   =     44867    247508
AFLR3 GG : Nodes, Elements   =     44867    246776
AFLR3 GG : Nodes, Elements   =     48214    256863
AFLR3 GG : Nodes, Elements   =     48214    271105
AFLR3 GG : Nodes, Elements   =     48214    267402
AFLR3 GG : Nodes, Elements   =     48214    266720
AFLR3 GG : Nodes, Elements   =     51448    276453
AFLR3 GG : Nodes, Elements   =     51448    290163
AFLR3 GG : Nodes, Elements   =     51448    286615
AFLR3 GG : Nodes, Elements   =     51448    286012
AFLR3 GG : Nodes, Elements   =     54543    295326
AFLR3 GG : Nodes, Elements   =     54543    308441
AFLR3 GG : Nodes, Elements   =     54543    305058
AFLR3 GG : Nodes, Elements   =     54543    304457
AFLR3 GG : Nodes, Elements   =     57499    313335
AFLR3 GG : Nodes, Elements   =     57499    325691
AFLR3 GG : Nodes, Elements   =     57499    322594
AFLR3 GG : Nodes, Elements   =     57499    322139
AFLR3 GG : Nodes, Elements   =     60348    330690
AFLR3 GG : Nodes, Elements   =     60348    342596
AFLR3 GG : Nodes, Elements   =     60348    339582
AFLR3 GG : Nodes, Elements   =     60348    339129
AFLR3 GG : Nodes, Elements   =     63012    347124
AFLR3 GG : Nodes, Elements   =     63012    358253
AFLR3 GG : Nodes, Elements   =     63012    355484
AFLR3 GG : Nodes, Elements   =     63012    355065
AFLR3 GG : Nodes, Elements   =     65481    362480
AFLR3 GG : Nodes, Elements   =     65481    372779
AFLR3 GG : Nodes, Elements   =     65481    370210
AFLR3 GG : Nodes, Elements   =     65481    369872
AFLR3 GG : Nodes, Elements   =     67716    376581
AFLR3 GG : Nodes, Elements   =     67716    385883
AFLR3 GG : Nodes, Elements   =     67716    383531
AFLR3 GG : Nodes, Elements   =     67716    383248
AFLR3 GG : Nodes, Elements   =     69605    388917
AFLR3 GG : Nodes, Elements   =     69605    396857
AFLR3 GG : Nodes, Elements   =     69605    394794
AFLR3 GG : Nodes, Elements   =     69605    394560
AFLR3 GG : Nodes, Elements   =     71085    399002
AFLR3 GG : Nodes, Elements   =     71085    405367
AFLR3 GG : Nodes, Elements   =     71085    403587
AFLR3 GG : Nodes, Elements   =     71085    403413
AFLR3 GG : Nodes, Elements   =     72213    406798
AFLR3 GG : Nodes, Elements   =     72213    411736
AFLR3 GG : Nodes, Elements   =     72213    410308
AFLR3 GG : Nodes, Elements   =     72213    410199
AFLR3 GG : Nodes, Elements   =     73020    412620
AFLR3 GG : Nodes, Elements   =     73020    416005
AFLR3 GG : Nodes, Elements   =     73020    415096
AFLR3 GG : Nodes, Elements   =     73020    414994
AFLR3 GG : Nodes, Elements   =     73572    416650
AFLR3 GG : Nodes, Elements   =     73572    419026
AFLR3 GG : Nodes, Elements   =     73572    418352
AFLR3 GG : Nodes, Elements   =     73572    418304
AFLR3 GG : Nodes, Elements   =     73906    419306
AFLR3 GG : Nodes, Elements   =     73906    420742
AFLR3 GG : Nodes, Elements   =     73906    420326
AFLR3 GG : Nodes, Elements   =     73906    420303
AFLR3 GG : Nodes, Elements   =     74075    420811
AFLR3 GG : Nodes, Elements   =     74075    421558
AFLR3 GG : Nodes, Elements   =     74075    421311
AFLR3 GG : Nodes, Elements   =     74075    421292
AFLR3 GG : Nodes, Elements   =     74166    421565
AFLR3 GG : Nodes, Elements   =     74166    421950
AFLR3 GG : Nodes, Elements   =     74166    421833
AFLR3 GG : Nodes, Elements   =     74166    421824
AFLR3 GG : Nodes, Elements   =     74210    421956
AFLR3 GG : Nodes, Elements   =     74210    422139
AFLR3 GG : Nodes, Elements   =     74210    422074
AFLR3 GG : Nodes, Elements   =     74210    422072
AFLR3 GG : Nodes, Elements   =     74220    422102
AFLR3 GG : Nodes, Elements   =     74220    422148
AFLR3 GG : Nodes, Elements   =     74220    422135
AFLR3 GG : Nodes, Elements   =     74220    422132
AFLR3 GG : Nodes, Elements   =     74224    422144
AFLR3 GG : Nodes, Elements   =     74224    422157
AFLR3 GG : Nodes, Elements   =     74224    422154
AFLR3 GG : Nodes, Elements   =     74247    422223
AFLR3 GG : Nodes, Elements   =     74247    422312
AFLR3 GG : Nodes, Elements   =     74247    422280
AFLR3 GG : Nodes, Elements   =     74247    422279
AFLR3 GG : Nodes, Elements   =     74253    422297
AFLR3 GG : Nodes, Elements   =     74253    422323
AFLR3 GG : Nodes, Elements   =     74253    422314
AFLR3 GG : Nodes, Elements   =     74253    422312
 
AFLR3    : CPU Time          =     6.875   seconds
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =     74253    422312
AFLR3 QI : Nodes, Elements   =     72809    414098
AFLR3 QI : Nodes, Elements   =     72576    412775
AFLR3 QI : Nodes, Elements   =     72556    412666
AFLR3 QI : Nodes, Elements   =     72555    412660
AFLR3 QI : Nodes, Elements   =     72555    416566
AFLR3 QI : Nodes, Elements   =     72555    412389
AFLR3 QI : Nodes, Elements   =     72555    411941
AFLR3 QI : Nodes, Elements   =     72555    412302
AFLR3 QI : Nodes, Elements   =     72555    411663
AFLR3 QI : Nodes, Elements   =     72555    411433
AFLR3 QI : Nodes, Elements   =     72555    411700
AFLR3 QI : Nodes, Elements   =     72555    411399
AFLR3 QI : Nodes, Elements   =     72555    411308
AFLR3 QI : Nodes, Elements   =     72555    411549
AFLR3 QI : Nodes, Elements   =     72555    411297
AFLR3 QI : Nodes, Elements   =     72555    411253
AFLR3 QI : Nodes, Elements   =     72555    411490
AFLR3 QI : Nodes, Elements   =     72555    411254
AFLR3 QI : Nodes, Elements   =     72555    411219
AFLR3 QI : Nodes, Elements   =     72558    411234
AFLR3 QI : Nodes, Elements   =     72558    411467
AFLR3 QI : Nodes, Elements   =     72558    411241
AFLR3 QI : Nodes, Elements   =     72558    411229
AFLR3 QI : Nodes, Elements   =     72558    411447
AFLR3 QI : Nodes, Elements   =     72558    411223
AFLR3 QI : Nodes, Elements   =     72558    411203
 
AFLR3    : CPU Time          =     2.289   seconds
 
AFLR3 QRG: QUALITY GRID RE-GENERATION
 
AFLR3 QRG: Nodes, Elements   =     72558    411203
AFLR3 QRG: Nodes, Elements   =     72563    411232
AFLR3 QRG: Nodes, Elements   =     72564    411237
AFLR3 QRG: Nodes, Elements   =     72568    411256
AFLR3 QRG: Nodes, Elements   =     72569    411263
 
AFLR3    : CPU Time          =     0.078   seconds
 
AFLR3    : DONE

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    411263
UG3      : Min, Max Ang      =    0.7896     177.7
UG3      : Average Angle     =      70.2
UG3      : No. Angle>160.0   =        58
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.12e+06

UG3      : No. Tet Elems     =    411263
UG3      : Min Vol           =  4.01e-10
UG3      : Average Vol       =      5.16
UG3      : Total-Tet-Vol     =  2.12e+06
UG3      : No. Vol<TOL       =         0

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

UG3      : No. Tet Elems     =    411263
UG3      : Min, Max Q        =    0.0428         1
UG3      : Average Q         =     0.893
UG3      : No. Q<       0.1  =        24
UG3      : No. Q<      0.01  =         0

OVERALL  : CPU Time          =     9.941   seconds

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    411263
UG3      : Min, Max Ang      =    0.7896     177.7
UG3      : Average Angle     =      70.2
UG3      : No. Angle>160.0   =        58
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.12e+06

UG3      : No. Tet Elems     =    411263
UG3      : Min Vol           =  4.01e-10
UG3      : Average Vol       =      5.16
UG3      : Total-Tet-Vol     =  2.12e+06
UG3      : No. Vol<TOL       =         0

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

UG3      : No. Tet Elems     =    411263
UG3      : Min, Max Q        =    0.0722         1
UG3      : Average Q         =     0.853
UG3      : No. Q<       0.1  =         1
UG3      : No. Q<      0.01  =         0

UG3      : CPU Time          =     0.000   seconds

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : CREATE EGADS TESS FROM AFLR3 DATA

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

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

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

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

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

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

EGADS    : EGADS TESS CREATED

EGADS    : CHECK TESS FACE NODE MAP

EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 9
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 10
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 16
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 17
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 18
Volume mesh:
	Number of nodes          = 72569
	Number of elements       = 423691
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 411263
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 72569
	Number of elements       = 423691
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 411263
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 72569
	Number of elements       = 423691
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 411263
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 72569
	Number of elements       = 423691
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 411263
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
ok
test_Multiple_Mesh (test_tetgen.TestTETGEN.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
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)
 7F0B5D59B740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F0B5D59B740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7F0B417B2700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F0B417B2700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Getting surface mesh for body 7 (of 7)
Body 1 (of 7)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 2 (of 7)
Number of nodes    = 296
Number of elements = 588
Number of triangle elements      = 588
Number of quadrilateral elements = 0
Body 3 (of 7)
Number of nodes    = 487
Number of elements = 970
Number of triangle elements      = 970
Number of quadrilateral elements = 0
Body 4 (of 7)
Number of nodes    = 2048
Number of elements = 4096
Number of triangle elements      = 4096
Number of quadrilateral elements = 0
Body 5 (of 7)
Number of nodes    = 152
Number of elements = 300
Number of triangle elements      = 300
Number of quadrilateral elements = 0
Body 6 (of 7)
Number of nodes    = 624
Number of elements = 1248
Number of triangle elements      = 1248
Number of quadrilateral elements = 0
Body 7 (of 7)
Number of nodes    = 488
Number of elements = 972
Number of triangle elements      = 972
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4193
Total number of elements = 8366
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 296, elements - 588
Body 3 number of surface: nodes - 487, elements - 970
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cylinder, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cone, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = torus, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = sphere, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = boxhole, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = bullet, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 296, elements - 588
Body 3 number of surface: nodes - 487, elements - 970
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Number of surface: nodes - 4193, elements - 8366
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_faceMatch_MultiDomain (test_tetgen.TestTETGEN.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 374
Number of elements = 744
Number of triangle elements      = 744
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 472
Total number of elements = 936
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 386
Number of elements = 768
Number of triangle elements      = 768
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 582
Total number of elements = 1152
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 351
Number of elements = 698
Number of triangle elements      = 698
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 491
Total number of elements = 970
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 376
Number of elements = 748
Number of triangle elements      = 748
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 516
Total number of elements = 1020
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 370
Number of elements = 736
Number of triangle elements      = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 454
Total number of elements = 896
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 370
Number of elements = 736
Number of triangle elements      = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 126
Number of elements = 252
Number of triangle elements      = 252
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 20
Number of elements = 36
Number of triangle elements      = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 516
Total number of elements = 1024
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 109
Number of elements = 214
Number of triangle elements      = 214
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 48
Number of elements = 96
Number of triangle elements      = 96
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 12
Number of elements = 20
Number of triangle elements      = 20
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 169
Total number of elements = 330
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 536
Number of elements = 1072
Number of triangle elements      = 1072
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 544
Number of elements = 1084
Number of triangle elements      = 1084
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 1080
Total number of elements = 2156
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 5)
Getting surface mesh for body 2 (of 5)
Getting surface mesh for body 3 (of 5)
Getting surface mesh for body 4 (of 5)
Getting surface mesh for body 5 (of 5)
Body 1 (of 5)
Number of nodes    = 1352
Number of elements = 2684
Number of triangle elements      = 2684
Number of quadrilateral elements = 0
Body 2 (of 5)
Number of nodes    = 288
Number of elements = 572
Number of triangle elements      = 572
Number of quadrilateral elements = 0
Body 3 (of 5)
Number of nodes    = 173
Number of elements = 342
Number of triangle elements      = 342
Number of quadrilateral elements = 0
Body 4 (of 5)
Number of nodes    = 26
Number of elements = 48
Number of triangle elements      = 48
Number of quadrilateral elements = 0
Body 5 (of 5)
Number of nodes    = 482
Number of elements = 960
Number of triangle elements      = 960
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 2321
Total number of elements = 4606
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1352, elements - 2684
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 173, elements - 342
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1352, elements - 2684
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 173, elements - 342
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 440
Number of elements = 876
Number of triangle elements      = 876
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 522
Number of elements = 1044
Number of triangle elements      = 1044
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 962
Total number of elements = 1920
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 440, elements - 876
Body 2 number of surface: nodes - 522, elements - 1044
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 440, elements - 876
Body 2 number of surface: nodes - 522, elements - 1044
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_journal (test_tetgen.TestTETGEN.test_journal) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
ok
test_phase (test_tetgen.TestTETGEN.test_phase) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 7130, elements - 14252
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_reenter (test_tetgen.TestTETGEN.test_reenter) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 9626
Number of elements = 19244
Number of triangle elements      = 19244
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9626
Total number of elements = 19244
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!

Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Binary STL file ....
Finished writing Binary STL file


Writing Tecplot file ....
Finished writing Tecplot file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing Binary VTK file ....
Finished writing Binary VTK file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!

Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Binary STL file ....
Finished writing Binary STL file


Writing Tecplot file ....
Finished writing Tecplot file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing Binary VTK file ....
Finished writing Binary VTK file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file

ok
test_setInput (test_tetgen.TestTETGEN.test_setInput) ...  EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_Cl (test_xfoil.Testxfoil_Kulfan.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_Kulfan.test_alpha_custom_increment) ... ok
test_CL_uniform_increment (test_xfoil.Testxfoil_NACA.test_CL_uniform_increment) ... ok
test_Cl (test_xfoil.Testxfoil_NACA.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_NACA.test_alpha_custom_increment) ... ok
test_alpha_uniform_inrement (test_xfoil.Testxfoil_NACA.test_alpha_uniform_inrement) ... ok
test_append (test_xfoil.Testxfoil_NACA.test_append) ... ok
test_normalize (test_xfoil.Testxfoil_NACA.test_normalize) ... ok
test_phase (test_xfoil.Testxfoil_NACA.test_phase) ... ok
test_Output (test_zaero.TestZAERO.test_Output) ... ok
test_inputs (test_zaero.TestZAERO.test_inputs) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 1220
Number of elements = 2680
Number of triangle elements      = 2680
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 1221
Total number of elements = 2680
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Rib_Root, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1220
	Number of elements = 2680
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 2680
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 1221
	Combined Number of elements = 2681
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 2680
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 6
	Property name - Rib_Root
	Property name - Rib_Root_Point
	Property name - Ribs
	Property name - Skin
	Property name - Spar1
	Property name - Spar2
	Done getting FEA properties
Updating mesh element types based on properties input

'Smart_Restart' is ON
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - WingSurface
	Done getting vortex lattice surface data
Getting vortex lattice control surface data
	VLM control surface name - CntrlLE
	VLM control surface name - CntrlTE
	Done getting vortex lattice control surface data

Getting FEA vortex lattice mesh

Getting ZAERO UAIC Configurations.......
	Number of UAIC Configurations - 2

	UAIC Configuration: climb, id = 1
	- Mach Number : 0.200000
	- Reduced Freq: [0.020000, ... , 0.250000]

	UAIC Configuration: cruise, id = 2
	- Mach Number : 0.700000
	- Reduced Freq: [0.040000, ... , 0.350000]

Getting ZAERO Analysis Subcases.......
	Number of Analysis Subcases - 2

	Analysis Subcase: FlutterCruise, id = 1
	- Discipline : flutter
	- UAIC       : cruise

	Analysis Subcase: Trim, id = 2
	- Discipline : Trim
	- UAIC       : climb

Getting ZAERO Trim Variables.......
	Number of Trim Variables - 2

	Trim Variable: ANGLEA
	- Label : ALPHA
	- Value : free

	Trim Variable: URDD3
	- Label : NZ
	- Value : 1.0

	Updating StaticAeroelastic subcase: Trim
	- vectorToCG -> [0.345898, 1.652951, -0.041403]
	- weight -> 476456.149985
	- weightMomentOfInertia -> [304902.643270, 98963.803820, 69822.813292, 6179.981375, 19723.152207, 370546.335524]
ok

----------------------------------------------------------------------
Ran 146 tests in 533.078s

OK (skipped=26)
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/
+ make test TYPE=MINIMAL
(make -C cCAPS -f aeroelastic_SU2.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'avlTest' is up to date.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'awaveTest' is up to date.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'frictionTest' is up to date.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: Nothing to be done for 'fun3d'.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f hsm.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'hsm' is up to date.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'interferenceTest' is up to date.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'msesTest' is up to date.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f mystran.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'mystranTest' is up to date.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'pointwiseTest' is up to date.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(cd ./regressionTest; ./execute_CTestRegression.sh MINIMAL)
Running.... MINIMAL c-Tests

All tests pass!

(cd ./regressionTest; ./execute_PyTestRegression.sh MINIMAL)

=================================================
Using python : /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python
=================================================

Running.... MINIMAL PyTests

=================================================
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ echo 'avl_PyTest.py test;'
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
CXtot   0.000611907868574681
CYtot   -6.289312383470904e-15
CZtot   -0.3012861394886091
Cltot   -4.782081713039163e-14
Cmtot   -0.1945055953450467
Cntot   -2.339461801636068e-15
Cl'tot  -4.7854363026524e-14
Cn'tot  -1.504517153549636e-15
CLtot   0.3012509314150773
CDtot   0.004646353488232845
CDvis   0.0
CLff    0.3009503023520526
CYff    -7.719145079534105e-15
CDind   0.004646353488232845
CDff    0.004968969500908293
e       0.9669902146157952
StripForces 
Wing  cl =  [0.02994790451347, 0.08555545178934, 0.1329003532588, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.310122128419, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805665, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996428, 0.2453427152623, 0.2100182422922, 0.1733025192801, 0.1329003532723, 0.08555545180788, 0.0299479045408]
Wing  cd =  [-0.004234137763162, -0.004494543653191, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946402, 0.0005114598078397, 0.0021191472861, 0.004145189908974, 0.006609094404182, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.00660909440444, 0.004145189909261, 0.002119147286385, 0.0005114598080999, -0.000738653894407, -0.001762021024095, -0.002739626801367, -0.003752887372445, -0.004494543653161, -0.004234137764545]

real	0m0.930s
user	0m0.717s
sys	0m0.435s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl =  [1.05475230552567, 1.36488869373635, 1.56607214272105, 2.03059709344879, 1.9727108312117, 1.87307153172386, 1.76050475760118]
Cd =  [0.0131991208675726, 0.0166540240605751, 0.0200551482562831, 0.045867134196922, 0.0754256009394857, 0.0994469174477521, 0.127479430989037]
Alpha =  [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0]
Transition location =  [0.496044114404284, 0.461377732041502, 0.44237656820185, 0.361251636355213, 0.276104140853559, 0.214381239321467, 0.132988264746663]

real	0m5.165s
user	0m4.844s
sys	0m0.288s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'mses_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl =  0.37837910855492196
Cd =  0.007775858417210155
Cm =  0.005262636995812415

real	0m5.114s
user	0m4.773s
sys	0m0.219s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'friction_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting Mach & Altitude Values
Lifting Surface: Body = 1, units m
	XLE:   1.571946 -3.872983 0.249728
	XTE:   2.536563 -3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 2, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.614012 0.000000 0.002015
	Chord: 1.614013
	Arc:   3.308635
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 3, units m
	XLE:   1.571946 3.872983 0.249728
	XTE:   2.536563 3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 4, units m
	XLE:   5.484123 0.000000 1.468246
	XTE:   6.210307 0.000915 1.468246
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 5, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.210307 0.001525 0.500000
	Chord: 1.210308
	Arc:   2.471195
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 6, units m
	XLE:   5.484123 -0.968246 0.500000
	XTE:   6.210307 -0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 7, units m
	XLE:   5.484123 0.968246 0.500000
	XTE:   6.210307 0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 8, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 9, units m
	Arc: 3.714180
	Diameter: 1.020621
	Type: Fuse
Body of Revolution: Body = 10, units m
	Arc: 2.771209
	Diameter: 0.645497
	Type: Fuse
Body of Revolution: Body = 11, units m
	Arc: 1.013945
	Diameter: 0.322749
	Type: Fuse
Body of Revolution: Body = 12, units m
	Arc: 0.101394
	Diameter: 0.032275
	Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2
Total drag = [0.0132, 0.01226]
Form drag = [0.0033, 0.00307]
Friction drag = [0.0099, 0.00919]

real	0m0.525s
user	0m0.482s
sys	0m0.284s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected)
=================================================


=================================================
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ echo 'egadsTess_PyTest.py test;'
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
	Name = Wing, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2

Getting mesh sizing parameters
	Mesh sizing name - LeadingEdge
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 4)
Getting surface mesh for body 2 (of 4)
Getting surface mesh for body 3 (of 4)
Getting surface mesh for body 4 (of 4)
Body 1 (of 4)
Number of nodes    = 3793
Number of elements = 4001
Number of triangle elements      = 0
Number of quadrilateral elements = 4001
Body 2 (of 4)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes    = 76
Number of elements = 55
Number of triangle elements      = 0
Number of quadrilateral elements = 55
Body 4 (of 4)
Number of nodes    = 100
Number of elements = 73
Number of triangle elements      = 0
Number of quadrilateral elements = 73
----------------------------
Total number of nodes    = 3970
Total number of elements = 4129

Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing ugrid file ....
Finished writing ugrid file


real	0m6.585s
user	0m13.791s
sys	0m0.994s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case egadsTess_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr2_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2    : Compile Date   04/23/24 @ 12:17PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       316       634
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       681      1018
AFLR2 GGp: Nodes, Faces      =      1013      1682
AFLR2 GGp: Nodes, Faces      =      1339      2334
AFLR2 GGp: Nodes, Faces      =      1652      2960
AFLR2 GGp: Nodes, Faces      =      1957      3570
AFLR2 GGp: Nodes, Faces      =      2252      4160
AFLR2 GGp: Nodes, Faces      =      2526      4708
AFLR2 GGp: Nodes, Faces      =      2809      5274
AFLR2 GGp: Nodes, Faces      =      3083      5822
AFLR2 GGp: Nodes, Faces      =      3327      6310
AFLR2 GGp: Nodes, Faces      =      3564      6784
AFLR2 GGp: Nodes, Faces      =      3788      7232
AFLR2 GGp: Nodes, Faces      =      3995      7646
AFLR2 GGp: Nodes, Faces      =      4194      8044
AFLR2 GGp: Nodes, Faces      =      4394      8444
AFLR2 GGp: Nodes, Faces      =      4585      8826
AFLR2 GGp: Nodes, Faces      =      4772      9200
AFLR2 GGp: Nodes, Faces      =      4943      9542
AFLR2 GGp: Nodes, Faces      =      5129      9914
AFLR2 GGp: Nodes, Faces      =      5293     10242
AFLR2 GGp: Nodes, Faces      =      5447     10550
AFLR2 GGp: Nodes, Faces      =      5594     10844
AFLR2 GGp: Nodes, Faces      =      5716     11088
AFLR2 GGp: Nodes, Faces      =      5830     11316
AFLR2 GGp: Nodes, Faces      =      5909     11474
AFLR2 GGp: Nodes, Faces      =      5964     11584
AFLR2 GGp: Nodes, Faces      =      6006     11668
AFLR2 GGp: Nodes, Faces      =      6025     11706
AFLR2 GGp: Nodes, Faces      =      6034     11724
 
AFLR2    : CPU Time          =     0.022   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      6034     11724
AFLR2 QI : Nodes, Faces      =      6033       454
AFLR2 QI : Nodes, Faces      =      6033      5634
AFLR2 QI : Nodes, Faces      =      6033     11722
AFLR2 QI : Nodes, Faces      =      6032       462
AFLR2 QI : Nodes, Faces      =      6032      5629
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6032       456
AFLR2 QI : Nodes, Faces      =      6032      5632
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6032       474
AFLR2 QI : Nodes, Faces      =      6032      5623
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6031       486
AFLR2 QI : Nodes, Faces      =      6031      5616
AFLR2 QI : Nodes, Faces      =      6031       488
AFLR2 QI : Nodes, Faces      =      6031      5616
 
AFLR2    : CPU Time          =     0.011   seconds
 
AFLR2    : DONE
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 6031
Number of elements = 6448
Number of tris = 488
Number of quad = 5616
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!

Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file


real	0m0.746s
user	0m0.758s
sys	0m0.375s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected)
=================================================


=================================================
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ echo 'aflr4_and_aflr3_PyTest.py test;'
aflr4_and_aflr3_PyTest.py test;
+ python -u aflr4_and_aflr3_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing ugrid file ....
Finished writing ugrid file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Wing1
	Mesh sizing name - Wing2
	Done getting mesh sizing parameters
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2    : Compile Date   04/23/24 @ 12:17PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR4    : Compile Date   04/23/24 @ 12:17PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 150512
	Number of elements       = 451696
	Number of triangles      = 14380
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 216264
	Number of pyramids       = 427
	Number of prisms         = 220625
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


real	0m16.474s
user	0m16.131s
sys	0m0.419s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'tetgen_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 2236
Number of elements = 4468
Number of triangle elements      = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 636
Number of elements = 1268
Number of triangle elements      = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 267
Number of elements = 530
Number of triangle elements      = 530
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 3139
Total number of elements = 6266

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 3139, elements - 6266
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.026185
Creating surface mesh ...
Surface mesh seconds:  0.007251
Recovering boundaries...
Boundary recovery seconds:  0.070942
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.013745
Suppressing Steiner points ...
Steiner suppression seconds:  3.1e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.014145
Refining mesh...
  4190 insertions, added 2180 points, 134280 tetrahedra in queue.
  1395 insertions, added 459 points, 138994 tetrahedra in queue.
  1859 insertions, added 487 points, 137112 tetrahedra in queue.
  2478 insertions, added 498 points, 120303 tetrahedra in queue.
  3304 insertions, added 499 points, 74342 tetrahedra in queue.
  4404 insertions, added 474 points, 460 tetrahedra in queue.
Refinement seconds:  0.869615
Smoothing vertices...
Mesh smoothing seconds:  0.649342
Improving mesh...
Mesh improvement seconds:  0.015156
Jettisoning redundant points.

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.004043
Total running seconds:  1.67068

Statistics:

  Input points: 3139
  Input facets: 6266
  Input segments: 9399
  Input holes: 2
  Input regions: 0

  Mesh points: 8309
  Mesh tetrahedra: 41161
  Mesh faces: 85455
  Mesh faces on exterior boundary: 6266
  Mesh faces on input facets: 6266
  Mesh edges on input segments: 9399
  Steiner points inside domain: 5170

Done meshing using TetGen!

Writing Tecplot file ....
Finished writing Tecplot file


real	0m2.963s
user	0m3.064s
sys	0m0.245s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case tetgen_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_and_AFLR2_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_PyTest.py test;
+ python -u su2_and_AFLR2_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Saving geometry
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2    : Compile Date   04/23/24 @ 12:17PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       545         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       545       545
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       110       222
AFLR2 IG : Nodes, Faces      =       220       442
AFLR2 IG : Nodes, Faces      =       330       662
AFLR2 IG : Nodes, Faces      =       440       882
AFLR2 IG : Nodes, Faces      =       517      1036
AFLR2 IG : Nodes, Faces      =       545      1092
AFLR2 IG : Nodes, Faces      =       549      1092
AFLR2 IG : Nodes, Faces      =       545       545
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       545       545
AFLR2 GGp: Nodes, Faces      =      1083      1621
AFLR2 GGp: Nodes, Faces      =      1616      2687
AFLR2 GGp: Nodes, Faces      =      2144      3743
AFLR2 GGp: Nodes, Faces      =      2661      4777
AFLR2 GGp: Nodes, Faces      =      3171      5797
AFLR2 GGp: Nodes, Faces      =      3672      6799
AFLR2 GGp: Nodes, Faces      =      4158      7771
AFLR2 GGp: Nodes, Faces      =      4653      8761
AFLR2 GGp: Nodes, Faces      =      5142      9739
AFLR2 GGp: Nodes, Faces      =      5608     10671
AFLR2 GGp: Nodes, Faces      =      6055     11565
AFLR2 GGp: Nodes, Faces      =      6482     12419
AFLR2 GGp: Nodes, Faces      =      6880     13215
AFLR2 GGp: Nodes, Faces      =      7257     13969
AFLR2 GGp: Nodes, Faces      =      7614     14683
AFLR2 GGp: Nodes, Faces      =      7947     15349
AFLR2 GGp: Nodes, Faces      =      8276     16007
AFLR2 GGp: Nodes, Faces      =      8575     16605
AFLR2 GGp: Nodes, Faces      =      8869     17193
AFLR2 GGp: Nodes, Faces      =      9140     17735
AFLR2 GGp: Nodes, Faces      =      9401     18257
AFLR2 GGp: Nodes, Faces      =      9654     18763
AFLR2 GGp: Nodes, Faces      =      9887     19229
AFLR2 GGp: Nodes, Faces      =     10110     19675
AFLR2 GGp: Nodes, Faces      =     10315     20085
AFLR2 GGp: Nodes, Faces      =     10497     20449
AFLR2 GGp: Nodes, Faces      =     10656     20767
AFLR2 GGp: Nodes, Faces      =     10791     21037
AFLR2 GGp: Nodes, Faces      =     10919     21293
AFLR2 GGp: Nodes, Faces      =     11022     21499
AFLR2 GGp: Nodes, Faces      =     11092     21639
AFLR2 GGp: Nodes, Faces      =     11145     21745
AFLR2 GGp: Nodes, Faces      =     11156     21767
 
AFLR2    : CPU Time          =     0.067   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     11156     21767
AFLR2 QI : Nodes, Faces      =     11155       819
AFLR2 QI : Nodes, Faces      =     11155     10473
AFLR2 QI : Nodes, Faces      =     11155     21765
AFLR2 QI : Nodes, Faces      =     11154       811
AFLR2 QI : Nodes, Faces      =     11154     10476
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11154       805
AFLR2 QI : Nodes, Faces      =     11154     10479
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11154       911
AFLR2 QI : Nodes, Faces      =     11154     10426
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11153       915
AFLR2 QI : Nodes, Faces      =     11153     10423
AFLR2 QI : Nodes, Faces      =     11153       917
AFLR2 QI : Nodes, Faces      =     11153     10423
 
AFLR2    : CPU Time          =     0.043   seconds
 
AFLR2    : DONE
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 11153
Number of elements = 11885
Number of tris = 917
Number of quad = 10423
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!

Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file


Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Airfoil
	Boundary condition name - InFlow
	Boundary condition name - OutFlow
	Boundary condition name - TunnelWall
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.

Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../aflr2/aflr2_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_su2_aflr2.dat.
Surface file name: surface_flow_pyCAPS_su2_aflr2.
Volume file name: flow_pyCAPS_su2_aflr2.
Restart file name: restart_flow_pyCAPS_su2_aflr2.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_5|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                     Inlet boundary|                               BC_4|
+-----------------------------------------------------------------------+
|                    Outlet boundary|                               BC_3|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
11153 grid points.
11340 volume elements.
4 surface markers.
98 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_4).
399 boundary elements in index 3 (Marker = BC_5).
917 triangles.
10423 quadrilaterals.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 917 TRIANGLE volume elements.
There has been a re-orientation of 10423 QUADRILATERAL volume elements.
There has been a re-orientation of 73 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.878.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 385.665. Mean K: 2.15881. Standard deviation K: 17.7215.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        49.3184|             90|
|     CV Face Area Aspect Ratio|        1.00035|        33.4982|
|           CV Sub-Volume Ratio|        1.00001|        7.89914|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11153|    1/1.00|        10|
|         1|      2702|    1/4.13|   7.38309|
|         2|       549|    1/4.92|   4.99198|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.06265 m.
Area projection in the x-plane = 0.211192 m, y-plane = 0.997011 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.102037 m.
Min. coordinate in the x-direction = 0.000323229 m, y-direction = -0.108492 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is NOT a single straight.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        216054|             1|   m^2/s^2|        216054|
|            Velocity-X|       136.119|             1|       m/s|       136.119|
|            Velocity-Y|             0|             1|       m/s|             0|
|    Velocity Magnitude|       136.119|             1|       m/s|       136.119|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|           0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.1161e-01|    0.071067|    2.739763|    1.616077|    5.599701|    0.055267|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.1788e-01|   -0.447576|    2.193837|    1.571349|    5.070382|    0.046028|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.1398e-01|   -0.561159|    2.074597|    1.490746|    4.953698|    0.033910|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.1034e-01|   -0.723326|    1.921155|    1.390756|    4.790278|    0.049695|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.0896e-01|   -0.876572|    1.825653|    1.275093|    4.637161|    0.133976|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.0853e-01|   -1.029177|    1.759196|    1.156078|    4.482282|    0.368542|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  1.0679e-01|   -1.215334|    1.704909|    1.114966|    4.286060|    0.974759|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  1.0588e-01|   -1.329970|    1.644937|    1.145030|    4.116982|    2.716332|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  1.0552e-01|   -1.270672|    1.570739|    1.155400|    4.139480|   16.569216|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  1.0495e-01|   -1.221243|    1.499646|    1.130319|    4.189559|   -6.277653|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.22124|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_su2_aflr2.dat  |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|CSV file                           |surface_flow_pyCAPS_su2_aflr2.csv  |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary                     |flow_pyCAPS_su2_aflr2.szplt        |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary surface             |surface_flow_pyCAPS_su2_aflr2.szplt|
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 994 more values.0: Error finishing Tecplot file output.

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------

Total Force - Pressure + Viscous
Cl =  0.072253 Cd =  -0.01151
Cmz =  0.070975
Cx =  -0.01151 Cy =  0.072253
Pressure Contribution
Cl_p =  0.072253 Cd_p =  -0.01151
Cmz_p =  0.070975
Cx_p =  -0.01151 Cy_p =  0.072253
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0

real	0m2.539s
user	0m2.361s
sys	0m0.486s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'masstran_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results mass properties.....

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 1159
Number of elements = 798
Number of triangle elements      = 0
Number of quadrilateral elements = 798
----------------------------
Total number of nodes    = 1159
Total number of elements = 798
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1159
	Number of elements = 798
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 798

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - Ribs_and_Spars
	No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
	Done getting FEA properties
Updating mesh element types based on properties input
Area      3.428666259747
Mass      5383.006027803
Centroid  [1.222256036874, 0.1634981473778, -4.234505810751e-11]
CG        [1.222256036874, 0.1634981473778, -4.234637807833e-11]
Ixx       22133.97306033
Iyy       23448.30046709
Izz       1389.213122582
Ixy       164.2055275657
Ixz       -7.45484669011e-06
Iyz       1.707686795832e-06
I         [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.45484669011e-06, 1.707686795832e-06]
II        [[22133.97306033, -164.2055275657, 7.45484669011e-06], [-164.2055275657, 23448.30046709, -1.707686795832e-06], [7.45484669011e-06, -1.707686795832e-06, 1389.213122582]]

real	0m4.552s
user	0m7.309s
sys	0m2.339s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating HSM BEM
	Getting quads for BEM!
	Number of nodal coordinates = 81
	Number of elements = 96
	Elemental Tria3 = 0
	Elemental Quad4 = 64

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Max Adjacency set to = 9
MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 32
->HSMSOL
 Matrix Non-zero Entries = 5741

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.130E-01  0.165E+00  0.153E-04    1.000  ddy @ (   0.25   0.06   0.00)
   1*   0.260E-03  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.12   0.00)
   1*   0.240E-05  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.09   0.00)
   2    0.379E-02  0.505E-01  0.750E-04    1.000  ddy @ (   0.25   0.19   0.00)
   2*   0.420E-04  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.12   0.00)
   3    0.168E-02  0.225E-01  0.208E-04    1.000  ddy @ (   0.25   0.06   0.00)
   4    0.325E-03  0.427E-02  0.250E-05    1.000  ddy @ (   0.25   0.19   0.00)
   5    0.794E-05  0.112E-03  0.170E-06    1.000  ddy @ (   0.25   0.19   0.00)
   6    0.387E-08  0.598E-07  0.197E-09    1.000  ddy @ (   0.25   0.06   0.00)
   7    0.848E-15  0.147E-13  0.924E-15    1.000  ddy @ (   0.25   0.19   0.00)

 Converging n vectors ...
 it =  1    dn =  0.788E-01   rlx = 1.000  (  59 )
 it =  2    dn =  0.566E-16   rlx = 1.000  (  35 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.691E-03   rlx = 1.000  (  45 )
 it =  2    de =  0.404E-04   rlx = 1.000  (   9 )
 it =  3    de =  0.142E-07   rlx = 1.000  (  46 )
 it =  4    de =  0.521E-11   rlx = 1.000  (  62 )

 Calculating  strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat

real	0m1.064s
user	0m1.049s
sys	0m0.329s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected)
=================================================


=================================================
+ echo '../corsairlite/qp.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
../corsairlite/qp.py test;
+ python -u ../corsairlite/qp.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   -21.56250 dimensionless

Variables
---------
   x  :  1.62500   [-]   The X variable
   y  :  1.37500   [-]   The Y variable

Constants
---------
   c   :  3         [-]   A constant
   c2  :  2         [-]   A constant

Sensitivities
-------------
   c   :  + 0.46957   A constant
   c2  :  - 0.22338   A constant

Solve Report
------------
   Solve Method           :  Quadratic Program 
   Classification         :  Convex 
   Solver                 :  cvxopt 


real	0m2.772s
user	0m2.870s
sys	0m0.790s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case ../corsairlite/qp.py passed (as expected)
=================================================


*************************************************
*************************************************

=================================================
Did not run examples for:

abaqus
awave
tsfoil
delaundo
Cart3D
Astros
Mystran
=================================================

All tests pass!

+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64
+ mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/test/plugs
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/test/plugs
+ sort -f
+ find /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/Plugs -name 'plugs0*.csm'
find: ‘/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/Plugs’: No such file or directory
+ awk '{ n=split($0, a, ";"); for(i=1; i<=n; i+=2) print a[i] }' /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/data/plugs/plugsFailure.txt
+ cp /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/data/plugs/plugsIgnore.txt .
+ set +x
Testing CSM files:
total 32M
-rw-rw-r--. 1 jenkins jenkins 1.3M Jun 25 23:03 ASTRO.D01
-rw-rw-r--. 1 jenkins jenkins 316K Jun 25 23:03 ASTRO.IDX
-rwxrwxr-x. 1 jenkins jenkins 1.1M Jun 25 23:03 avl
-rwxrwxr-x. 1 jenkins jenkins  41K Jun 25 23:02 egads2cart
-rwxrwxr-x. 1 jenkins jenkins 140K Jun 25 23:04 egads2cgt
-rwxrwxr-x. 1 jenkins jenkins  54K Jun 25 23:04 friction
-rwxrwxr-x. 1 jenkins jenkins 8.2M Jun 25 23:03 mastros.exe
-rwxrwxr-x. 1 jenkins jenkins 727K Jun 25 23:03 mses
-rwxrwxr-x. 1 jenkins jenkins 536K Jun 25 23:03 mset
-rwxrwxr-x. 1 jenkins jenkins  51K Jun 25 23:03 phaseUtil
-rw-rw-r--. 1 jenkins jenkins 1.6K Jun 25 23:06 pod.egads
-rw-rw-r--. 1 jenkins jenkins    0 Jun 25 23:06 port7681.jrnl
-rwxrwxr-x. 1 jenkins jenkins 451K Jun 25 23:03 pplot
-rwxrwxr-x. 1 jenkins jenkins 405K Jun 25 23:03 pxplot
-rwxrwxr-x. 1 jenkins jenkins 143K Jun 25 23:02 sensCSM
-rwxrwxr-x. 1 jenkins jenkins 624K Jun 25 23:02 serveCSM
-rwxrwxr-x. 1 jenkins jenkins 537K Jun 25 23:02 serveESP
-rwxrwxr-x. 1 jenkins jenkins 719K Jun 25 23:03 Slugs
-rwxrwxr-x. 1 jenkins jenkins 210K Jun 25 23:03 TestFit
-rwxrwxr-x. 1 jenkins jenkins  78K Jun 25 23:02 vCurvature
-rwxrwxr-x. 1 jenkins jenkins  50K Jun 25 23:02 vGeom
-rwxrwxr-x. 1 jenkins jenkins  80K Jun 25 23:02 vTess
-rwxrwxr-x. 1 jenkins jenkins  15M Jun 25 23:02 vTesstatic
-rw-rw-r--. 1 jenkins jenkins 195K Jun 25 23:06 wingMultiModel.bdf
-rwxrwxr-x. 1 jenkins jenkins 1.1M Jun 25 23:03 xfoil
[Execution node] check if [reynolds-centOS8] is in [[viggen]]
Run condition [Execution node ] preventing perform for step [Execute shell]
[Execution node] check if [reynolds-centOS8] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_Beta/CASREV=7.8,ESP_ARCH=LINUX64,buildnode=reynolds-centOS8 #732'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS