Started by upstream project "ESP_Beta" build number 720
originally caused by:
Started by remote host 18.18.33.14
Running as SYSTEM
[EnvInject] - Loading node environment variables.
Building remotely on reynolds-centOS8 in workspace /home/jenkins/workspace/ESP_Beta/7.7/LINUX64
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
Checking out a fresh workspace because there's no workspace at /home/jenkins/workspace/ESP_Beta/7.7/LINUX64
Cleaning local Directory .
Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-05-30T12:18:09.796 -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 2501
Checking out a fresh workspace because /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/JenkinsESP doesn't exist
Cleaning local Directory JenkinsESP
Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-05-30T12:18:09.796 -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 863
No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
No changes for svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP since the previous build
[GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[Execution node] check if [reynolds-centOS8] is in [[macys, macys_VM, reynolds, reynolds-centOS7, reynolds-centOS8, reynolds-ubuntu18]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[LINUX64] $ /bin/bash -ex /tmp/jenkins12394654992103660991.sh
+ bash -ex /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/JenkinsESP/ESP_Beta.sh
+ source /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.8
++ 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 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
++++++ new_dirs=
++++++ read -r install_path
++++++ unset G_MESSAGES_DEBUG
++++++ echo /home/jenkins/.local/share/flatpak
++++++ GIO_USE_VFS=local
++++++ flatpak --installations
++++++ share_path=/home/jenkins/.local/share/flatpak/exports/share
++++++ case ":$XDG_DATA_DIRS:" in
++++++ :
++++++ read -r install_path
++++++ share_path=/var/lib/flatpak/exports/share
++++++ case ":$XDG_DATA_DIRS:" in
++++++ :
++++++ read -r install_path
++++++ echo ''
+++++ new_dirs=
+++++ export XDG_DATA_DIRS
+++++ XDG_DATA_DIRS=/home/jenkins/.local/share/flatpak/exports/share:/var/lib/flatpak/exports/share:/usr/local/share:/usr/share
++++ for i in /etc/profile.d/*.sh
++++ '[' -r /etc/profile.d/gawk.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/gawk.sh
++++ for i in /etc/profile.d/*.sh
++++ '[' -r /etc/profile.d/gnome-ssh-askpass.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/gnome-ssh-askpass.sh
+++++ SSH_ASKPASS=/usr/libexec/openssh/gnome-ssh-askpass
+++++ export SSH_ASKPASS
++++ for i in /etc/profile.d/*.sh
++++ '[' -r /etc/profile.d/lang.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/lang.sh
+++++ '[' -n en_US.UTF-8 ']'
+++++ LANG_backup=en_US.UTF-8
+++++ for config in /etc/locale.conf "${HOME}/.i18n"
+++++ '[' -f /etc/locale.conf ']'
++++++ /usr/bin/sed -r -e 's/^[[:blank:]]*([[:upper:]_]+)=([[:print:][:digit:]\._-]+|"[[:print:][:digit:]\._-]+")/export \1=\2/;t;d' /etc/locale.conf
+++++ eval export 'LANG="en_US.UTF-8"'
++++++ export LANG=en_US.UTF-8
++++++ LANG=en_US.UTF-8
+++++ for config in /etc/locale.conf "${HOME}/.i18n"
+++++ '[' -f /home/jenkins/.i18n ']'
+++++ '[' -n en_US.UTF-8 ']'
+++++ LANG=en_US.UTF-8
+++++ unset LANG_backup config
+++++ '[' -n '' ']'
+++++ '[' -n en_US.UTF-8 ']'
+++++ '[' dumb = linux ']'
++++ for i in /etc/profile.d/*.sh
++++ '[' -r /etc/profile.d/less.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/less.sh
+++++ '[' -z '||/usr/bin/lesspipe.sh %s' ']'
++++ for i in /etc/profile.d/*.sh
++++ '[' -r /etc/profile.d/PackageKit.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/PackageKit.sh
+++++ [[ -n '' ]]
++++ for i in /etc/profile.d/*.sh
++++ '[' -r /etc/profile.d/ssh-x-forwarding.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/ssh-x-forwarding.sh
+++++ '[' -z '18.18.33.14 44802 172.16.90.130 22' ']'
+++++ '[' -z 1 ']'
+++++ '[' -z '' ']'
+++++ return
++++ for i in /etc/profile.d/*.sh
++++ '[' -r /etc/profile.d/vim.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/vim.sh
+++++ '[' -n '4.4.20(1)-release' -o -n '' -o -n '' ']'
++++++ /usr/bin/id -u
+++++ '[' 1001 -le 200 ']'
+++++ alias vi
+++++ alias vi=vim
++++ for i in /etc/profile.d/*.sh
++++ '[' -r /etc/profile.d/vte.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/vte.sh
+++++ '[' -n '4.4.20(1)-release' -o -n '' ']'
+++++ [[ ehxB == *i* ]]
+++++ return 0
++++ for i in /etc/profile.d/*.sh
++++ '[' -r /etc/profile.d/which2.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/which2.sh
+++++ case "$(basename $(readlink /proc/$$/exe))" in
+++++++ readlink /proc/1695842/exe
++++++ basename /usr/bin/bash
+++++ which_declare='declare -f'
+++++ which_opt=-f
+++++ export which_declare
+++++ export -f which
++++ unset i
++++ unset -f pathmunge
+++ PATH=/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
+++ export PATH
++ export CAPS_OUTLEVEL=0
++ CAPS_OUTLEVEL=0
++ [[ LINUX64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64
++ ESP_BLOC=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64
++ export ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64
++ ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64
++ export JULIA_DEPOT_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/julia
++ JULIA_DEPOT_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.8 != '' ]]
++ [[ '' != '' ]]
++ [[ 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-7.7.0
++ export CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.7.0
++ CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.7.0
++ export CASARCH=.
++ CASARCH=.
++ export LD_LIBRARY_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ LD_LIBRARY_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ export ESP_EXTERN_LIBS=/home/jenkins/util/ESP/ExternLibs
++ ESP_EXTERN_LIBS=/home/jenkins/util/ESP/ExternLibs
++ export AFLR=/home/jenkins/util/AFLR/aflr_lib_11.5.14
++ AFLR=/home/jenkins/util/AFLR/aflr_lib_11.5.14
++ export AFLR_ARCH=Linux-x86-64
++ AFLR_ARCH=Linux-x86-64
++ export PATH=/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ PATH=/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ export CART3D=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16
++ CART3D=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16
++ export CART3D_ARCH=X86_64_ICC
++ CART3D_ARCH=X86_64_ICC
++ export PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ export PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ export PATH=/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ PATH=/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ export PATH=/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ PATH=/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ export MYSTRAN_directory=/home/jenkins/util/mystran/MYSTRAN/Binaries
++ MYSTRAN_directory=/home/jenkins/util/mystran/MYSTRAN/Binaries
++ export PATH=/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ PATH=/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ export PATH=/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ PATH=/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ export CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/CAPS/aim/pointwise/glyph
++ export PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin
++ [[ reynolds-centOS8 == \r\e\y\n\o\l\d\s ]]
++ export SU2_HOME=/home/jenkins/util/SU2/SU2-v8.0.0
++ SU2_HOME=/home/jenkins/util/SU2/SU2-v8.0.0
++ export SU2_RUN=/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ SU2_RUN=/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ export PATH=/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ '[' -d /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16 ']'
++ export PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ [[ reynolds-centOS8 == \m\a\c\y\s* ]]
++ [[ reynolds-centOS8 == \v\i\g\g\e\n ]]
+++ python-config --includes
++ export 'PYTHONINC=. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
++ PYTHONINC='. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
+++ python-config --help
++ [[ Usage: /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python-config --prefix|--exec-prefix|--includes|--libs|--cflags|--ldflags|--extension-suffix|--help|--abiflags|--configdir|--embed == *\e\m\b\e\d* ]]
+++ python-config --ldflags --embed
++ export 'PYTHONLIB= -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lpthread -ldl -lutil -lm '
++ PYTHONLIB=' -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lpthread -ldl -lutil -lm '
++ [[ reynolds-centOS8 == \m\a\c\y\s ]]
++ [[ reynolds-centOS8 == \v\i\g\g\e\n ]]
++ export PYTHONUNBUFFERED=true
++ PYTHONUNBUFFERED=true
++ export PYTHONFAULTHANDLER=true
++ PYTHONFAULTHANDLER=true
++ python --version
Python 3.11.9
++ [[ LINUX64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export CSMDATA=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/data
++ CSMDATA=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/data
+ virtualenv /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv
created virtual environment CPython3.11.9.final.0-64 in 557ms
creator CPython3Posix(dest=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv, clear=False, no_vcs_ignore=False, global=False)
seeder FromAppData(download=False, pip=bundle, setuptools=bundle, wheel=bundle, via=copy, app_data_dir=/home/jenkins/.local/share/virtualenv)
added seed packages: pip==24.0, setuptools==69.5.1, wheel==0.43.0
activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator
+ . /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/activate
++ '[' /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/activate = /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/JenkinsESP/ESP_Beta.sh ']'
++ deactivate nondestructive
++ unset -f pydoc
++ '[' -z '' ']'
++ '[' -z '' ']'
++ hash -r
++ '[' -z '' ']'
++ unset VIRTUAL_ENV
++ unset VIRTUAL_ENV_PROMPT
++ '[' '!' nondestructive = nondestructive ']'
++ VIRTUAL_ENV=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv
++ '[' linux-gnu = cygwin ']'
++ '[' linux-gnu = msys ']'
++ export VIRTUAL_ENV
++ _OLD_VIRTUAL_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH
++ '[' x '!=' x ']'
+++ basename /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv
++ VIRTUAL_ENV_PROMPT=ESP_venv
++ export VIRTUAL_ENV_PROMPT
++ '[' -z _ ']'
++ _OLD_VIRTUAL_PYTHONHOME=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9
++ unset PYTHONHOME
++ '[' -z '' ']'
++ _OLD_VIRTUAL_PS1=
++ PS1='(ESP_venv) '
++ export PS1
++ alias pydoc
++ true
++ hash -r
+ pip_install pip
+ /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade pip
Requirement already satisfied: pip in ./ESP_venv/lib/python3.11/site-packages (24.0)
+ pip_install f90nml
+ /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade f90nml
Collecting f90nml
Using cached f90nml-1.4.4-py2.py3-none-any.whl.metadata (6.0 kB)
Using cached f90nml-1.4.4-py2.py3-none-any.whl (32 kB)
Installing collected packages: f90nml
Successfully installed f90nml-1.4.4
+ pip_install numpy
+ /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade numpy
Collecting numpy
Using cached numpy-1.26.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (61 kB)
Using cached numpy-1.26.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (18.3 MB)
Installing collected packages: numpy
Successfully installed numpy-1.26.4
+ pip_install openmdao
+ /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade openmdao
Collecting openmdao
Using cached openmdao-3.32.0-py3-none-any.whl
Collecting networkx>=2.0 (from openmdao)
Using cached networkx-3.3-py3-none-any.whl.metadata (5.1 kB)
Requirement already satisfied: numpy<2 in ./ESP_venv/lib/python3.11/site-packages (from openmdao) (1.26.4)
Collecting packaging (from openmdao)
Using cached packaging-24.0-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-1.13.1-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 urllib3-2.2.1-py3-none-any.whl.metadata (6.4 kB)
Collecting certifi>=2017.4.17 (from requests->openmdao)
Using cached certifi-2024.2.2-py3-none-any.whl.metadata (2.2 kB)
Using cached networkx-3.3-py3-none-any.whl (1.7 MB)
Using cached packaging-24.0-py3-none-any.whl (53 kB)
Downloading requests-2.32.3-py3-none-any.whl (64 kB)
━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━ 64.9/64.9 kB 4.0 MB/s eta 0:00:00
Using cached scipy-1.13.1-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (38.6 MB)
Using cached certifi-2024.2.2-py3-none-any.whl (163 kB)
Using cached charset_normalizer-3.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (140 kB)
Using cached idna-3.7-py3-none-any.whl (66 kB)
Using cached urllib3-2.2.1-py3-none-any.whl (121 kB)
Installing collected packages: urllib3, scipy, packaging, networkx, idna, charset-normalizer, certifi, requests, openmdao
Successfully installed certifi-2024.2.2 charset-normalizer-3.3.2 idna-3.7 networkx-3.3 openmdao-3.32.0 packaging-24.0 requests-2.32.3 scipy-1.13.1 urllib3-2.2.1
+ [[ reynolds-centOS8 == *\v\i\g\g\e\n* ]]
+ pip_install cvxopt
+ /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade cvxopt
Collecting cvxopt
Using cached cvxopt-1.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (1.3 kB)
Using cached cvxopt-1.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (13.6 MB)
Installing collected packages: cvxopt
Successfully installed cvxopt-1.3.2
+ pip_install dill
+ /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade dill
Collecting dill
Using cached dill-0.3.8-py3-none-any.whl.metadata (10 kB)
Using cached dill-0.3.8-py3-none-any.whl (116 kB)
Installing collected packages: dill
Successfully installed dill-0.3.8
+ pip_install packaging
+ /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade packaging
Requirement already satisfied: packaging in ./ESP_venv/lib/python3.11/site-packages (24.0)
+ pip_install matplotlib
+ /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade matplotlib
Collecting matplotlib
Using cached matplotlib-3.9.0-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-4.52.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (161 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) (24.0)
Collecting pillow>=8 (from matplotlib)
Using cached pillow-10.3.0-cp311-cp311-manylinux_2_28_x86_64.whl.metadata (9.2 kB)
Collecting pyparsing>=2.3.1 (from matplotlib)
Using cached pyparsing-3.1.2-py3-none-any.whl.metadata (5.1 kB)
Collecting python-dateutil>=2.7 (from matplotlib)
Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl.metadata (8.4 kB)
Collecting six>=1.5 (from python-dateutil>=2.7->matplotlib)
Using cached six-1.16.0-py2.py3-none-any.whl.metadata (1.8 kB)
Using cached matplotlib-3.9.0-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-4.52.4-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-4.52.4 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/7.7/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade scipy
Requirement already satisfied: scipy in ./ESP_venv/lib/python3.11/site-packages (1.13.1)
Requirement already satisfied: numpy<2.3,>=1.22.4 in ./ESP_venv/lib/python3.11/site-packages (from scipy) (1.26.4)
+ unset PYTHONINC
+ unset PYTHONLIB
+ unset UDUNITS2_XML_PATH
+ unset ESP_BLOC
+ unset ESP_ROOT
+ unset ESP_ARCH
+ unset AWAVE
+ unset AFLR
+ unset AFLR_ARCH
+ wget --tries=3 https://acdl.mit.edu/ESP/archive/ESPbeta.tgz
--2024-05-30 12:18:52-- 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: 272121672 (260M) [application/x-gzip]
Saving to: ‘ESPbeta.tgz’
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13050K .......... .......... .......... .......... .......... 4% 12.8M 15s
13100K .......... .......... .......... .......... .......... 4% 15.9M 15s
13150K .......... .......... .......... .......... .......... 4% 16.2M 15s
13200K .......... .......... .......... .......... .......... 4% 16.3M 15s
13250K .......... .......... .......... .......... .......... 5% 9.28M 15s
13300K .......... .......... .......... .......... .......... 5% 13.8M 15s
13350K .......... .......... .......... .......... .......... 5% 15.9M 15s
13400K .......... .......... .......... .......... .......... 5% 7.92M 15s
13450K .......... .......... .......... .......... .......... 5% 14.5M 15s
13500K .......... .......... .......... .......... .......... 5% 7.48M 15s
13550K .......... .......... .......... .......... .......... 5% 11.4M 15s
13600K .......... .......... .......... .......... .......... 5% 12.3M 15s
13650K .......... .......... .......... .......... .......... 5% 10.6M 15s
13700K .......... .......... .......... .......... .......... 5% 15.2M 15s
13750K .......... .......... .......... .......... .......... 5% 23.3M 15s
13800K .......... .......... .......... .......... .......... 5% 29.7M 15s
13850K .......... .......... .......... .......... .......... 5% 10.1M 15s
13900K .......... .......... .......... .......... .......... 5% 13.3M 15s
13950K .......... .......... .......... .......... .......... 5% 4.76M 15s
14000K .......... .......... .......... .......... .......... 5% 6.74M 16s
14050K .......... .......... .......... .......... .......... 5% 13.3M 16s
14100K .......... .......... .......... .......... .......... 5% 12.0M 16s
14150K .......... .......... .......... .......... .......... 5% 10.4M 16s
14200K .......... .......... .......... .......... .......... 5% 13.2M 16s
14250K .......... .......... .......... .......... .......... 5% 13.4M 16s
14300K .......... .......... .......... .......... .......... 5% 10.6M 16s
14350K .......... .......... .......... .......... .......... 5% 7.76M 16s
14400K .......... .......... .......... .......... .......... 5% 13.2M 16s
14450K .......... .......... .......... .......... .......... 5% 20.6M 16s
14500K .......... .......... .......... .......... .......... 5% 18.7M 16s
14550K .......... .......... .......... .......... .......... 5% 10.5M 16s
14600K .......... .......... .......... .......... .......... 5% 7.24M 16s
14650K .......... .......... .......... .......... .......... 5% 15.1M 16s
14700K .......... .......... .......... .......... .......... 5% 9.28M 16s
14750K .......... .......... .......... .......... .......... 5% 16.8M 16s
14800K .......... .......... .......... .......... .......... 5% 19.7M 16s
14850K .......... .......... .......... .......... .......... 5% 13.0M 16s
14900K .......... .......... .......... .......... .......... 5% 19.3M 16s
14950K .......... .......... .......... .......... .......... 5% 12.0M 16s
15000K .......... .......... .......... .......... .......... 5% 14.3M 16s
15050K .......... .......... .......... .......... .......... 5% 21.1M 16s
15100K .......... .......... .......... .......... .......... 5% 17.4M 16s
15150K .......... .......... .......... .......... .......... 5% 10.3M 16s
15200K .......... .......... .......... .......... .......... 5% 15.7M 16s
15250K .......... .......... .......... .......... .......... 5% 12.5M 16s
15300K .......... .......... .......... .......... .......... 5% 12.1M 16s
15350K .......... .......... .......... .......... .......... 5% 19.4M 16s
15400K .......... .......... .......... .......... .......... 5% 16.0M 16s
15450K .......... .......... .......... .......... .......... 5% 15.1M 16s
15500K .......... .......... .......... .......... .......... 5% 3.83M 16s
15550K .......... .......... .......... .......... .......... 5% 114M 16s
15600K .......... .......... .......... .......... .......... 5% 78.9M 16s
15650K .......... .......... .......... .......... .......... 5% 174M 16s
15700K .......... .......... .......... .......... .......... 5% 82.8M 16s
15750K .......... .......... .......... .......... .......... 5% 93.1M 16s
15800K .......... .......... .......... .......... .......... 5% 31.4M 16s
15850K .......... .......... .......... .......... .......... 5% 10.2M 16s
15900K .......... .......... .......... .......... .......... 6% 18.9M 16s
15950K .......... .......... .......... .......... .......... 6% 13.6M 16s
16000K .......... .......... .......... .......... .......... 6% 13.8M 16s
16050K .......... .......... .......... .......... .......... 6% 21.5M 16s
16100K .......... .......... .......... .......... .......... 6% 12.7M 16s
16150K .......... .......... .......... .......... .......... 6% 12.7M 16s
16200K .......... .......... .......... .......... .......... 6% 17.2M 16s
16250K .......... .......... .......... .......... .......... 6% 13.2M 16s
16300K .......... .......... .......... .......... .......... 6% 10.7M 16s
16350K .......... .......... .......... .......... .......... 6% 13.0M 16s
16400K .......... .......... .......... .......... .......... 6% 19.9M 16s
16450K .......... .......... .......... .......... .......... 6% 7.48M 16s
16500K .......... .......... .......... .......... .......... 6% 25.8M 16s
16550K .......... .......... .......... .......... .......... 6% 14.2M 16s
16600K .......... .......... .......... .......... .......... 6% 8.63M 16s
16650K .......... .......... .......... .......... .......... 6% 17.1M 16s
16700K .......... .......... .......... .......... .......... 6% 15.2M 16s
16750K .......... .......... .......... .......... .......... 6% 12.6M 16s
16800K .......... .......... .......... .......... .......... 6% 23.8M 16s
16850K .......... .......... .......... .......... .......... 6% 13.3M 16s
16900K .......... .......... .......... .......... .......... 6% 19.8M 16s
16950K .......... .......... .......... .......... .......... 6% 14.8M 16s
17000K .......... .......... .......... .......... .......... 6% 14.4M 16s
17050K .......... .......... .......... .......... .......... 6% 15.8M 16s
17100K .......... .......... .......... .......... .......... 6% 11.9M 16s
17150K .......... .......... .......... .......... .......... 6% 11.7M 16s
17200K .......... .......... .......... .......... .......... 6% 24.8M 16s
17250K .......... .......... .......... .......... .......... 6% 9.87M 16s
17300K .......... .......... .......... .......... .......... 6% 15.9M 16s
17350K .......... .......... .......... .......... .......... 6% 12.2M 16s
17400K .......... .......... .......... .......... .......... 6% 11.6M 16s
17450K .......... .......... .......... .......... .......... 6% 11.8M 16s
17500K .......... .......... .......... .......... .......... 6% 11.9M 16s
17550K .......... .......... .......... .......... .......... 6% 21.7M 16s
17600K .......... .......... .......... .......... .......... 6% 11.9M 16s
17650K .......... .......... .......... .......... .......... 6% 12.1M 16s
17700K .......... .......... .......... .......... .......... 6% 19.2M 16s
17750K .......... .......... .......... .......... .......... 6% 15.4M 16s
17800K .......... .......... .......... .......... .......... 6% 13.5M 16s
17850K .......... .......... .......... .......... .......... 6% 28.7M 16s
17900K .......... .......... .......... .......... .......... 6% 13.9M 16s
17950K .......... .......... .......... .......... .......... 6% 11.0M 16s
18000K .......... .......... .......... .......... .......... 6% 37.2M 16s
18050K .......... .......... .......... .......... .......... 6% 25.5M 16s
18100K .......... .......... .......... .......... .......... 6% 8.05M 16s
18150K .......... .......... .......... .......... .......... 6% 58.1M 16s
18200K .......... .......... .......... .......... .......... 6% 23.0M 16s
18250K .......... .......... .......... .......... .......... 6% 13.5M 16s
18300K .......... .......... .......... .......... .......... 6% 12.7M 16s
18350K .......... .......... .......... .......... .......... 6% 38.9M 16s
18400K .......... .......... .......... .......... .......... 6% 11.7M 16s
18450K .......... .......... .......... .......... .......... 6% 11.2M 16s
18500K .......... .......... .......... .......... .......... 6% 64.9M 16s
18550K .......... .......... .......... .......... .......... 6% 18.5M 16s
18600K .......... .......... .......... .......... .......... 7% 7.26M 16s
18650K .......... .......... .......... .......... .......... 7% 83.1M 16s
18700K .......... .......... .......... .......... .......... 7% 23.7M 16s
18750K .......... .......... .......... .......... .......... 7% 10.6M 16s
18800K .......... .......... .......... .......... .......... 7% 14.5M 16s
18850K .......... .......... .......... .......... .......... 7% 40.3M 16s
18900K .......... .......... .......... .......... .......... 7% 24.5M 16s
18950K .......... .......... .......... .......... .......... 7% 6.74M 16s
19000K .......... .......... .......... .......... .......... 7% 108M 16s
19050K .......... .......... .......... .......... .......... 7% 23.6M 16s
19100K .......... .......... .......... .......... .......... 7% 8.33M 16s
19150K .......... .......... .......... .......... .......... 7% 15.3M 16s
19200K .......... .......... .......... .......... .......... 7% 24.8M 16s
19250K .......... .......... .......... .......... .......... 7% 15.8M 16s
19300K .......... .......... .......... .......... .......... 7% 8.86M 16s
19350K .......... .......... .......... .......... .......... 7% 37.5M 16s
19400K .......... .......... .......... .......... .......... 7% 22.7M 16s
19450K .......... .......... .......... .......... .......... 7% 9.57M 16s
19500K .......... .......... .......... .......... .......... 7% 14.3M 16s
19550K .......... .......... .......... .......... .......... 7% 27.9M 16s
19600K .......... .......... .......... .......... .......... 7% 14.5M 16s
19650K .......... .......... .......... .......... .......... 7% 8.95M 16s
19700K .......... .......... .......... .......... .......... 7% 27.7M 16s
19750K .......... .......... .......... .......... .......... 7% 20.3M 16s
19800K .......... .......... .......... .......... .......... 7% 12.2M 16s
19850K .......... .......... .......... .......... .......... 7% 14.8M 16s
19900K .......... .......... .......... .......... .......... 7% 28.9M 16s
19950K .......... .......... .......... .......... .......... 7% 12.9M 16s
20000K .......... .......... .......... .......... .......... 7% 10.9M 16s
20050K .......... .......... .......... .......... .......... 7% 28.0M 16s
20100K .......... .......... .......... .......... .......... 7% 19.5M 16s
20150K .......... .......... .......... .......... .......... 7% 12.4M 16s
20200K .......... .......... .......... .......... .......... 7% 13.4M 16s
20250K .......... .......... .......... .......... .......... 7% 26.1M 16s
20300K .......... .......... .......... .......... .......... 7% 27.4M 16s
20350K .......... .......... .......... .......... .......... 7% 7.58M 16s
20400K .......... .......... .......... .......... .......... 7% 28.9M 16s
20450K .......... .......... .......... .......... .......... 7% 21.7M 16s
20500K .......... .......... .......... .......... .......... 7% 9.07M 16s
20550K .......... .......... .......... .......... .......... 7% 21.7M 16s
20600K .......... .......... .......... .......... .......... 7% 17.4M 16s
20650K .......... .......... .......... .......... .......... 7% 19.4M 16s
20700K .......... .......... .......... .......... .......... 7% 12.3M 16s
20750K .......... .......... .......... .......... .......... 7% 21.0M 16s
20800K .......... .......... .......... .......... .......... 7% 21.2M 15s
20850K .......... .......... .......... .......... .......... 7% 9.80M 16s
20900K .......... .......... .......... .......... .......... 7% 30.1M 15s
20950K .......... .......... .......... .......... .......... 7% 13.8M 15s
21000K .......... .......... .......... .......... .......... 7% 15.4M 15s
21050K .......... .......... .......... .......... .......... 7% 12.1M 15s
21100K .......... .......... .......... .......... .......... 7% 24.4M 15s
21150K .......... .......... .......... .......... .......... 7% 21.9M 15s
21200K .......... .......... .......... .......... .......... 7% 9.22M 15s
21250K .......... .......... .......... .......... .......... 8% 26.9M 15s
21300K .......... .......... .......... .......... .......... 8% 14.7M 15s
21350K .......... .......... .......... .......... .......... 8% 21.6M 15s
21400K .......... .......... .......... .......... .......... 8% 10.0M 15s
21450K .......... .......... .......... .......... .......... 8% 18.6M 15s
21500K .......... .......... .......... .......... .......... 8% 22.9M 15s
21550K .......... .......... .......... .......... .......... 8% 16.2M 15s
21600K .......... .......... .......... .......... .......... 8% 11.3M 15s
21650K .......... .......... .......... .......... .......... 8% 15.1M 15s
21700K .......... .......... .......... .......... .......... 8% 14.6M 15s
21750K .......... .......... .......... .......... .......... 8% 14.2M 15s
21800K .......... .......... .......... .......... .......... 8% 16.0M 15s
21850K .......... .......... .......... .......... .......... 8% 18.5M 15s
21900K .......... .......... .......... .......... .......... 8% 20.1M 15s
21950K .......... .......... .......... .......... .......... 8% 9.32M 15s
22000K .......... .......... .......... .......... .......... 8% 20.1M 15s
22050K .......... .......... .......... .......... .......... 8% 17.3M 15s
22100K .......... .......... .......... .......... .......... 8% 13.8M 15s
22150K .......... .......... .......... .......... .......... 8% 12.7M 15s
22200K .......... .......... .......... .......... .......... 8% 19.0M 15s
22250K .......... .......... .......... .......... .......... 8% 14.2M 15s
22300K .......... .......... .......... .......... .......... 8% 16.0M 15s
22350K .......... .......... .......... .......... .......... 8% 11.0M 15s
22400K .......... .......... .......... .......... .......... 8% 18.6M 15s
22450K .......... .......... .......... .......... .......... 8% 16.5M 15s
22500K .......... .......... .......... .......... .......... 8% 14.2M 15s
22550K .......... .......... .......... .......... .......... 8% 15.5M 15s
22600K .......... .......... .......... .......... .......... 8% 14.9M 15s
22650K .......... .......... .......... .......... .......... 8% 15.5M 15s
22700K .......... .......... .......... .......... .......... 8% 9.93M 15s
22750K .......... .......... .......... .......... .......... 8% 18.2M 15s
22800K .......... .......... .......... .......... .......... 8% 21.0M 15s
22850K .......... .......... .......... .......... .......... 8% 21.7M 15s
22900K .......... .......... .......... .......... .......... 8% 10.5M 15s
22950K .......... .......... .......... .......... .......... 8% 12.2M 15s
23000K .......... .......... .......... .......... .......... 8% 25.3M 15s
23050K .......... .......... .......... .......... .......... 8% 16.5M 15s
23100K .......... .......... .......... .......... .......... 8% 9.44M 15s
23150K .......... .......... .......... .......... .......... 8% 19.3M 15s
23200K .......... .......... .......... .......... .......... 8% 15.5M 15s
23250K .......... .......... .......... .......... .......... 8% 21.0M 15s
23300K .......... .......... .......... .......... .......... 8% 11.5M 15s
23350K .......... .......... .......... .......... .......... 8% 13.2M 15s
23400K .......... .......... .......... .......... .......... 8% 25.9M 15s
23450K .......... .......... .......... .......... .......... 8% 10.5M 15s
23500K .......... .......... .......... .......... .......... 8% 10.9M 15s
23550K .......... .......... .......... .......... .......... 8% 41.0M 15s
23600K .......... .......... .......... .......... .......... 8% 20.9M 15s
23650K .......... .......... .......... .......... .......... 8% 10.8M 15s
23700K .......... .......... .......... .......... .......... 8% 13.4M 15s
23750K .......... .......... .......... .......... .......... 8% 17.8M 15s
23800K .......... .......... .......... .......... .......... 8% 22.5M 15s
23850K .......... .......... .......... .......... .......... 8% 10.4M 15s
23900K .......... .......... .......... .......... .......... 9% 12.8M 15s
23950K .......... .......... .......... .......... .......... 9% 17.4M 15s
24000K .......... .......... .......... .......... .......... 9% 25.6M 15s
24050K .......... .......... .......... .......... .......... 9% 12.9M 15s
24100K .......... .......... .......... .......... .......... 9% 11.0M 15s
24150K .......... .......... .......... .......... .......... 9% 22.0M 15s
24200K .......... .......... .......... .......... .......... 9% 13.9M 15s
24250K .......... .......... .......... .......... .......... 9% 20.6M 15s
24300K .......... .......... .......... .......... .......... 9% 11.6M 15s
24350K .......... .......... .......... .......... .......... 9% 19.0M 15s
24400K .......... .......... .......... .......... .......... 9% 15.2M 15s
24450K .......... .......... .......... .......... .......... 9% 9.65M 15s
24500K .......... .......... .......... .......... .......... 9% 14.9M 15s
24550K .......... .......... .......... .......... .......... 9% 41.4M 15s
24600K .......... .......... .......... .......... .......... 9% 11.0M 15s
24650K .......... .......... .......... .......... .......... 9% 14.7M 15s
24700K .......... .......... .......... .......... .......... 9% 13.0M 15s
24750K .......... .......... .......... .......... .......... 9% 28.0M 15s
24800K .......... .......... .......... .......... .......... 9% 13.2M 15s
24850K .......... .......... .......... .......... .......... 9% 10.8M 15s
24900K .......... .......... .......... .......... .......... 9% 15.0M 15s
24950K .......... .......... .......... .......... .......... 9% 27.1M 15s
25000K .......... .......... .......... .......... .......... 9% 12.9M 15s
25050K .......... .......... .......... .......... .......... 9% 12.9M 15s
25100K .......... .......... .......... .......... .......... 9% 11.7M 15s
25150K .......... .......... .......... .......... .......... 9% 28.4M 15s
25200K .......... .......... .......... .......... .......... 9% 12.8M 15s
25250K .......... .......... .......... .......... .......... 9% 10.3M 15s
25300K .......... .......... .......... .......... .......... 9% 19.1M 15s
25350K .......... .......... .......... .......... .......... 9% 18.2M 15s
25400K .......... .......... .......... .......... .......... 9% 16.0M 15s
25450K .......... .......... .......... .......... .......... 9% 10.1M 15s
25500K .......... .......... .......... .......... .......... 9% 18.4M 15s
25550K .......... .......... .......... .......... .......... 9% 21.6M 15s
25600K .......... .......... .......... .......... .......... 9% 14.5M 15s
25650K .......... .......... .......... .......... .......... 9% 10.8M 15s
25700K .......... .......... .......... .......... .......... 9% 15.8M 15s
25750K .......... .......... .......... .......... .......... 9% 15.4M 15s
25800K .......... .......... .......... .......... .......... 9% 21.3M 15s
25850K .......... .......... .......... .......... .......... 9% 9.99M 15s
25900K .......... .......... .......... .......... .......... 9% 23.5M 15s
25950K .......... .......... .......... .......... .......... 9% 13.6M 15s
26000K .......... .......... .......... .......... .......... 9% 14.7M 15s
26050K .......... .......... .......... .......... .......... 9% 17.1M 15s
26100K .......... .......... .......... .......... .......... 9% 12.1M 15s
26150K .......... .......... .......... .......... .......... 9% 20.4M 15s
26200K .......... .......... .......... .......... .......... 9% 10.4M 15s
26250K .......... .......... .......... .......... .......... 9% 26.6M 15s
26300K .......... .......... .......... .......... .......... 9% 15.0M 15s
26350K .......... .......... .......... .......... .......... 9% 13.5M 15s
26400K .......... .......... .......... .......... .......... 9% 12.6M 15s
26450K .......... .......... .......... .......... .......... 9% 26.7M 15s
26500K .......... .......... .......... .......... .......... 9% 14.9M 15s
26550K .......... .......... .......... .......... .......... 10% 13.1M 15s
26600K .......... .......... .......... .......... .......... 10% 12.1M 15s
26650K .......... .......... .......... .......... .......... 10% 21.2M 15s
26700K .......... .......... .......... .......... .......... 10% 11.7M 15s
26750K .......... .......... .......... .......... .......... 10% 18.9M 15s
26800K .......... .......... .......... .......... .......... 10% 13.9M 15s
26850K .......... .......... .......... .......... .......... 10% 23.5M 15s
26900K .......... .......... .......... .......... .......... 10% 11.3M 15s
26950K .......... .......... .......... .......... .......... 10% 13.3M 15s
27000K .......... .......... .......... .......... .......... 10% 17.5M 15s
27050K .......... .......... .......... .......... .......... 10% 24.0M 15s
27100K .......... .......... .......... .......... .......... 10% 9.75M 15s
27150K .......... .......... .......... .......... .......... 10% 18.7M 15s
27200K .......... .......... .......... .......... .......... 10% 15.2M 15s
27250K .......... .......... .......... .......... .......... 10% 28.7M 15s
27300K .......... .......... .......... .......... .......... 10% 11.2M 15s
27350K .......... .......... .......... .......... .......... 10% 17.4M 15s
27400K .......... .......... .......... .......... .......... 10% 17.3M 15s
27450K .......... .......... .......... .......... .......... 10% 9.32M 15s
27500K .......... .......... .......... .......... .......... 10% 21.5M 15s
27550K .......... .......... .......... .......... .......... 10% 21.7M 15s
27600K .......... .......... .......... .......... .......... 10% 15.4M 15s
27650K .......... .......... .......... .......... .......... 10% 9.95M 15s
27700K .......... .......... .......... .......... .......... 10% 22.7M 15s
27750K .......... .......... .......... .......... .......... 10% 22.5M 15s
27800K .......... .......... .......... .......... .......... 10% 16.4M 15s
27850K .......... .......... .......... .......... .......... 10% 21.7M 15s
27900K .......... .......... .......... .......... .......... 10% 9.91M 15s
27950K .......... .......... .......... .......... .......... 10% 18.8M 15s
28000K .......... .......... .......... .......... .......... 10% 18.2M 15s
28050K .......... .......... .......... .......... .......... 10% 32.1M 15s
28100K .......... .......... .......... .......... .......... 10% 9.07M 15s
28150K .......... .......... .......... .......... .......... 10% 22.2M 15s
28200K .......... .......... .......... .......... .......... 10% 13.5M 15s
28250K .......... .......... .......... .......... .......... 10% 35.7M 15s
28300K .......... .......... .......... .......... .......... 10% 10.9M 15s
28350K .......... .......... .......... .......... .......... 10% 13.5M 15s
28400K .......... .......... .......... .......... .......... 10% 16.4M 15s
28450K .......... .......... .......... .......... .......... 10% 38.8M 15s
28500K .......... .......... .......... .......... .......... 10% 9.81M 15s
28550K .......... .......... .......... .......... .......... 10% 27.9M 15s
28600K .......... .......... .......... .......... .......... 10% 10.3M 15s
28650K .......... .......... .......... .......... .......... 10% 68.7M 15s
28700K .......... .......... .......... .......... .......... 10% 7.92M 15s
28750K .......... .......... .......... .......... .......... 10% 34.0M 15s
28800K .......... .......... .......... .......... .......... 10% 18.9M 15s
28850K .......... .......... .......... .......... .......... 10% 14.5M 15s
28900K .......... .......... .......... .......... .......... 10% 8.31M 15s
28950K .......... .......... .......... .......... .......... 10% 45.5M 15s
29000K .......... .......... .......... .......... .......... 10% 21.3M 15s
29050K .......... .......... .......... .......... .......... 10% 16.2M 15s
29100K .......... .......... .......... .......... .......... 10% 9.19M 15s
29150K .......... .......... .......... .......... .......... 10% 22.6M 15s
29200K .......... .......... .......... .......... .......... 11% 23.0M 15s
29250K .......... .......... .......... .......... .......... 11% 14.7M 15s
29300K .......... .......... .......... .......... .......... 11% 9.63M 15s
29350K .......... .......... .......... .......... .......... 11% 25.2M 15s
29400K .......... .......... .......... .......... .......... 11% 26.0M 15s
29450K .......... .......... .......... .......... .......... 11% 14.5M 15s
29500K .......... .......... .......... .......... .......... 11% 8.18M 15s
29550K .......... .......... .......... .......... .......... 11% 24.5M 15s
29600K .......... .......... .......... .......... .......... 11% 25.2M 15s
29650K .......... .......... .......... .......... .......... 11% 15.2M 15s
29700K .......... .......... .......... .......... .......... 11% 8.61M 15s
29750K .......... .......... .......... .......... .......... 11% 31.1M 15s
29800K .......... .......... .......... .......... .......... 11% 32.1M 15s
29850K .......... .......... .......... .......... .......... 11% 13.2M 15s
29900K .......... .......... .......... .......... .......... 11% 23.2M 15s
29950K .......... .......... .......... .......... .......... 11% 9.24M 15s
30000K .......... .......... .......... .......... .......... 11% 39.9M 15s
30050K .......... .......... .......... .......... .......... 11% 24.5M 15s
30100K .......... .......... .......... .......... .......... 11% 12.2M 15s
30150K .......... .......... .......... .......... .......... 11% 9.77M 15s
30200K .......... .......... .......... .......... .......... 11% 35.2M 15s
30250K .......... .......... .......... .......... .......... 11% 26.4M 15s
30300K .......... .......... .......... .......... .......... 11% 13.6M 15s
30350K .......... .......... .......... .......... .......... 11% 8.71M 15s
30400K .......... .......... .......... .......... .......... 11% 39.5M 15s
30450K .......... .......... .......... .......... .......... 11% 20.0M 15s
30500K .......... .......... .......... .......... .......... 11% 15.8M 15s
30550K .......... .......... .......... .......... .......... 11% 9.56M 15s
30600K .......... .......... .......... .......... .......... 11% 24.5M 15s
30650K .......... .......... .......... .......... .......... 11% 35.2M 15s
30700K .......... .......... .......... .......... .......... 11% 12.4M 15s
30750K .......... .......... .......... .......... .......... 11% 36.0M 15s
30800K .......... .......... .......... .......... .......... 11% 8.60M 15s
30850K .......... .......... .......... .......... .......... 11% 75.8M 15s
30900K .......... .......... .......... .......... .......... 11% 13.6M 15s
30950K .......... .......... .......... .......... .......... 11% 17.1M 15s
31000K .......... .......... .......... .......... .......... 11% 9.42M 15s
31050K .......... .......... .......... .......... .......... 11% 60.5M 15s
31100K .......... .......... .......... .......... .......... 11% 20.7M 15s
31150K .......... .......... .......... .......... .......... 11% 14.7M 15s
31200K .......... .......... .......... .......... .......... 11% 8.45M 15s
31250K .......... .......... .......... .......... .......... 11% 35.4M 15s
31300K .......... .......... .......... .......... .......... 11% 23.4M 15s
31350K .......... .......... .......... .......... .......... 11% 16.1M 15s
31400K .......... .......... .......... .......... .......... 11% 20.1M 15s
31450K .......... .......... .......... .......... .......... 11% 9.13M 15s
31500K .......... .......... .......... .......... .......... 11% 37.2M 15s
31550K .......... .......... .......... .......... .......... 11% 17.8M 15s
31600K .......... .......... .......... .......... .......... 11% 15.5M 15s
31650K .......... .......... .......... .......... .......... 11% 9.36M 15s
31700K .......... .......... .......... .......... .......... 11% 43.0M 15s
31750K .......... .......... .......... .......... .......... 11% 24.8M 15s
31800K .......... .......... .......... .......... .......... 11% 14.9M 15s
31850K .......... .......... .......... .......... .......... 12% 8.17M 15s
31900K .......... .......... .......... .......... .......... 12% 44.4M 15s
31950K .......... .......... .......... .......... .......... 12% 26.0M 15s
32000K .......... .......... .......... .......... .......... 12% 12.1M 15s
32050K .......... .......... .......... .......... .......... 12% 10.3M 15s
32100K .......... .......... .......... .......... .......... 12% 22.2M 15s
32150K .......... .......... .......... .......... .......... 12% 27.9M 15s
32200K .......... .......... .......... .......... .......... 12% 13.4M 15s
32250K .......... .......... .......... .......... .......... 12% 26.2M 15s
32300K .......... .......... .......... .......... .......... 12% 8.84M 15s
32350K .......... .......... .......... .......... .......... 12% 29.9M 15s
32400K .......... .......... .......... .......... .......... 12% 23.0M 15s
32450K .......... .......... .......... .......... .......... 12% 14.8M 15s
32500K .......... .......... .......... .......... .......... 12% 8.94M 15s
32550K .......... .......... .......... .......... .......... 12% 35.0M 15s
32600K .......... .......... .......... .......... .......... 12% 16.2M 15s
32650K .......... .......... .......... .......... .......... 12% 17.8M 15s
32700K .......... .......... .......... .......... .......... 12% 19.4M 15s
32750K .......... .......... .......... .......... .......... 12% 11.0M 15s
32800K .......... .......... .......... .......... .......... 12% 32.8M 15s
32850K .......... .......... .......... .......... .......... 12% 12.0M 15s
32900K .......... .......... .......... .......... .......... 12% 28.1M 15s
32950K .......... .......... .......... .......... .......... 12% 8.25M 15s
33000K .......... .......... .......... .......... .......... 12% 29.2M 15s
33050K .......... .......... .......... .......... .......... 12% 25.2M 15s
33100K .......... .......... .......... .......... .......... 12% 18.6M 15s
33150K .......... .......... .......... .......... .......... 12% 10.5M 15s
33200K .......... .......... .......... .......... .......... 12% 2.89M 15s
33250K .......... .......... .......... .......... .......... 12% 336M 15s
33300K .......... .......... .......... .......... .......... 12% 153M 15s
33350K .......... .......... .......... .......... .......... 12% 145M 15s
33400K .......... .......... .......... .......... .......... 12% 193M 15s
33450K .......... .......... .......... .......... .......... 12% 87.8M 15s
33500K .......... .......... .......... .......... .......... 12% 36.2M 15s
33550K .......... .......... .......... .......... .......... 12% 8.98M 15s
33600K .......... .......... .......... .......... .......... 12% 16.2M 15s
33650K .......... .......... .......... .......... .......... 12% 14.4M 15s
33700K .......... .......... .......... .......... .......... 12% 3.81M 15s
33750K .......... .......... .......... .......... .......... 12% 49.6M 15s
33800K .......... .......... .......... .......... .......... 12% 40.4M 15s
33850K .......... .......... .......... .......... .......... 12% 39.6M 15s
33900K .......... .......... .......... .......... .......... 12% 15.4M 15s
33950K .......... .......... .......... .......... .......... 12% 8.34M 15s
34000K .......... .......... .......... .......... .......... 12% 11.0M 15s
34050K .......... .......... .......... .......... .......... 12% 28.2M 15s
34100K .......... .......... .......... .......... .......... 12% 7.31M 15s
34150K .......... .......... .......... .......... .......... 12% 15.3M 15s
34200K .......... .......... .......... .......... .......... 12% 7.49M 15s
34250K .......... .......... .......... .......... .......... 12% 15.1M 15s
34300K .......... .......... .......... .......... .......... 12% 7.98M 15s
34350K .......... .......... .......... .......... .......... 12% 13.1M 15s
34400K .......... .......... .......... .......... .......... 12% 8.07M 15s
34450K .......... .......... .......... .......... .......... 12% 13.2M 15s
34500K .......... .......... .......... .......... .......... 13% 11.3M 15s
34550K .......... .......... .......... .......... .......... 13% 14.0M 15s
34600K .......... .......... .......... .......... .......... 13% 8.79M 15s
34650K .......... .......... .......... .......... .......... 13% 11.9M 15s
34700K .......... .......... .......... .......... .......... 13% 8.28M 15s
34750K .......... .......... .......... .......... .......... 13% 11.9M 15s
34800K .......... .......... .......... .......... .......... 13% 14.2M 15s
34850K .......... .......... .......... .......... .......... 13% 9.47M 15s
34900K .......... .......... .......... .......... .......... 13% 17.5M 15s
34950K .......... .......... .......... .......... .......... 13% 7.07M 15s
35000K .......... .......... .......... .......... .......... 13% 15.9M 15s
35050K .......... .......... .......... .......... .......... 13% 6.85M 15s
35100K .......... .......... .......... .......... .......... 13% 14.5M 15s
35150K .......... .......... .......... .......... .......... 13% 13.3M 15s
35200K .......... .......... .......... .......... .......... 13% 7.37M 15s
35250K .......... .......... .......... .......... .......... 13% 15.0M 15s
35300K .......... .......... .......... .......... .......... 13% 11.1M 15s
35350K .......... .......... .......... .......... .......... 13% 14.2M 15s
35400K .......... .......... .......... .......... .......... 13% 7.27M 15s
35450K .......... .......... .......... .......... .......... 13% 14.3M 15s
35500K .......... .......... .......... .......... .......... 13% 15.1M 15s
35550K .......... .......... .......... .......... .......... 13% 8.21M 15s
35600K .......... .......... .......... .......... .......... 13% 13.6M 15s
35650K .......... .......... .......... .......... .......... 13% 10.3M 15s
35700K .......... .......... .......... .......... .......... 13% 10.9M 15s
35750K .......... .......... .......... .......... .......... 13% 10.4M 15s
35800K .......... .......... .......... .......... .......... 13% 11.2M 15s
35850K .......... .......... .......... .......... .......... 13% 15.7M 15s
35900K .......... .......... .......... .......... .......... 13% 7.16M 15s
35950K .......... .......... .......... .......... .......... 13% 15.8M 15s
36000K .......... .......... .......... .......... .......... 13% 10.9M 15s
36050K .......... .......... .......... .......... .......... 13% 12.9M 15s
36100K .......... .......... .......... .......... .......... 13% 10.1M 15s
36150K .......... .......... .......... .......... .......... 13% 9.00M 15s
36200K .......... .......... .......... .......... .......... 13% 12.5M 15s
36250K .......... .......... .......... .......... .......... 13% 8.46M 15s
36300K .......... .......... .......... .......... .......... 13% 17.7M 15s
36350K .......... .......... .......... .......... .......... 13% 13.3M 15s
36400K .......... .......... .......... .......... .......... 13% 8.64M 15s
36450K .......... .......... .......... .......... .......... 13% 10.8M 15s
36500K .......... .......... .......... .......... .......... 13% 9.68M 15s
36550K .......... .......... .......... .......... .......... 13% 17.0M 15s
36600K .......... .......... .......... .......... .......... 13% 13.4M 15s
36650K .......... .......... .......... .......... .......... 13% 8.69M 15s
36700K .......... .......... .......... .......... .......... 13% 9.51M 15s
36750K .......... .......... .......... .......... .......... 13% 21.2M 15s
36800K .......... .......... .......... .......... .......... 13% 7.62M 15s
36850K .......... .......... .......... .......... .......... 13% 16.2M 15s
36900K .......... .......... .......... .......... .......... 13% 8.87M 15s
36950K .......... .......... .......... .......... .......... 13% 10.2M 15s
37000K .......... .......... .......... .......... .......... 13% 18.6M 15s
37050K .......... .......... .......... .......... .......... 13% 7.86M 15s
37100K .......... .......... .......... .......... .......... 13% 17.0M 15s
37150K .......... .......... .......... .......... .......... 13% 9.03M 15s
37200K .......... .......... .......... .......... .......... 14% 9.27M 15s
37250K .......... .......... .......... .......... .......... 14% 72.5M 15s
37300K .......... .......... .......... .......... .......... 14% 7.54M 15s
37350K .......... .......... .......... .......... .......... 14% 12.3M 15s
37400K .......... .......... .......... .......... .......... 14% 9.66M 15s
37450K .......... .......... .......... .......... .......... 14% 8.90M 15s
37500K .......... .......... .......... .......... .......... 14% 38.0M 15s
37550K .......... .......... .......... .......... .......... 14% 7.12M 15s
37600K .......... .......... .......... .......... .......... 14% 10.9M 15s
37650K .......... .......... .......... .......... .......... 14% 9.82M 15s
37700K .......... .......... .......... .......... .......... 14% 9.36M 15s
37750K .......... .......... .......... .......... .......... 14% 34.7M 15s
37800K .......... .......... .......... .......... .......... 14% 6.88M 15s
37850K .......... .......... .......... .......... .......... 14% 13.2M 15s
37900K .......... .......... .......... .......... .......... 14% 19.3M 15s
37950K .......... .......... .......... .......... .......... 14% 6.11M 15s
38000K .......... .......... .......... .......... .......... 14% 32.2M 15s
38050K .......... .......... .......... .......... .......... 14% 9.45M 15s
38100K .......... .......... .......... .......... .......... 14% 8.90M 15s
38150K .......... .......... .......... .......... .......... 14% 25.4M 15s
38200K .......... .......... .......... .......... .......... 14% 5.78M 15s
38250K .......... .......... .......... .......... .......... 14% 39.5M 15s
38300K .......... .......... .......... .......... .......... 14% 9.99M 15s
38350K .......... .......... .......... .......... .......... 14% 8.74M 15s
38400K .......... .......... .......... .......... .......... 14% 28.2M 15s
38450K .......... .......... .......... .......... .......... 14% 7.07M 15s
38500K .......... .......... .......... .......... .......... 14% 20.0M 15s
38550K .......... .......... .......... .......... .......... 14% 23.4M 15s
38600K .......... .......... .......... .......... .......... 14% 7.63M 15s
38650K .......... .......... .......... .......... .......... 14% 57.6M 15s
38700K .......... .......... .......... .......... .......... 14% 7.11M 15s
38750K .......... .......... .......... .......... .......... 14% 17.0M 15s
38800K .......... .......... .......... .......... .......... 14% 29.3M 15s
38850K .......... .......... .......... .......... .......... 14% 7.73M 15s
38900K .......... .......... .......... .......... .......... 14% 13.3M 15s
38950K .......... .......... .......... .......... .......... 14% 13.9M 15s
39000K .......... .......... .......... .......... .......... 14% 9.44M 15s
39050K .......... .......... .......... .......... .......... 14% 13.8M 15s
39100K .......... .......... .......... .......... .......... 14% 13.2M 15s
39150K .......... .......... .......... .......... .......... 14% 7.87M 15s
39200K .......... .......... .......... .......... .......... 14% 10.7M 15s
39250K .......... .......... .......... .......... .......... 14% 14.2M 15s
39300K .......... .......... .......... .......... .......... 14% 12.0M 15s
39350K .......... .......... .......... .......... .......... 14% 9.76M 15s
39400K .......... .......... .......... .......... .......... 14% 12.2M 15s
39450K .......... .......... .......... .......... .......... 14% 13.2M 15s
39500K .......... .......... .......... .......... .......... 14% 13.9M 15s
39550K .......... .......... .......... .......... .......... 14% 14.4M 15s
39600K .......... .......... .......... .......... .......... 14% 8.30M 15s
39650K .......... .......... .......... .......... .......... 14% 16.0M 15s
39700K .......... .......... .......... .......... .......... 14% 8.98M 15s
39750K .......... .......... .......... .......... .......... 14% 19.9M 15s
39800K .......... .......... .......... .......... .......... 14% 12.0M 15s
39850K .......... .......... .......... .......... .......... 15% 11.2M 15s
39900K .......... .......... .......... .......... .......... 15% 13.7M 15s
39950K .......... .......... .......... .......... .......... 15% 13.0M 15s
40000K .......... .......... .......... .......... .......... 15% 11.9M 15s
40050K .......... .......... .......... .......... .......... 15% 8.45M 15s
40100K .......... .......... .......... .......... .......... 15% 9.57M 15s
40150K .......... .......... .......... .......... .......... 15% 12.9M 15s
40200K .......... .......... .......... .......... .......... 15% 10.3M 15s
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40300K .......... .......... .......... .......... .......... 15% 11.4M 15s
40350K .......... .......... .......... .......... .......... 15% 12.2M 15s
40400K .......... .......... .......... .......... .......... 15% 15.7M 15s
40450K .......... .......... .......... .......... .......... 15% 13.6M 15s
40500K .......... .......... .......... .......... .......... 15% 10.4M 15s
40550K .......... .......... .......... .......... .......... 15% 13.9M 15s
40600K .......... .......... .......... .......... .......... 15% 11.5M 15s
40650K .......... .......... .......... .......... .......... 15% 12.1M 15s
40700K .......... .......... .......... .......... .......... 15% 14.0M 15s
40750K .......... .......... .......... .......... .......... 15% 12.2M 15s
40800K .......... .......... .......... .......... .......... 15% 12.4M 15s
40850K .......... .......... .......... .......... .......... 15% 9.74M 15s
40900K .......... .......... .......... .......... .......... 15% 14.9M 15s
40950K .......... .......... .......... .......... .......... 15% 9.82M 15s
41000K .......... .......... .......... .......... .......... 15% 12.8M 15s
41050K .......... .......... .......... .......... .......... 15% 14.7M 15s
41100K .......... .......... .......... .......... .......... 15% 11.8M 15s
41150K .......... .......... .......... .......... .......... 15% 13.3M 15s
41200K .......... .......... .......... .......... .......... 15% 12.9M 15s
41250K .......... .......... .......... .......... .......... 15% 8.69M 15s
41300K .......... .......... .......... .......... .......... 15% 10.1M 15s
41350K .......... .......... .......... .......... .......... 15% 20.4M 15s
41400K .......... .......... .......... .......... .......... 15% 15.1M 15s
41450K .......... .......... .......... .......... .......... 15% 9.07M 15s
41500K .......... .......... .......... .......... .......... 15% 20.9M 15s
41550K .......... .......... .......... .......... .......... 15% 16.7M 15s
41600K .......... .......... .......... .......... .......... 15% 7.08M 15s
41650K .......... .......... .......... .......... .......... 15% 12.4M 15s
41700K .......... .......... .......... .......... .......... 15% 7.36M 15s
41750K .......... .......... .......... .......... .......... 15% 8.08M 15s
41800K .......... .......... .......... .......... .......... 15% 12.1M 15s
41850K .......... .......... .......... .......... .......... 15% 22.0M 15s
41900K .......... .......... .......... .......... .......... 15% 8.31M 15s
41950K .......... .......... .......... .......... .......... 15% 7.36M 15s
42000K .......... .......... .......... .......... .......... 15% 11.6M 15s
42050K .......... .......... .......... .......... .......... 15% 11.8M 15s
42100K .......... .......... .......... .......... .......... 15% 9.67M 15s
42150K .......... .......... .......... .......... .......... 15% 12.0M 15s
42200K .......... .......... .......... .......... .......... 15% 8.11M 15s
42250K .......... .......... .......... .......... .......... 15% 14.3M 15s
42300K .......... .......... .......... .......... .......... 15% 20.1M 15s
42350K .......... .......... .......... .......... .......... 15% 9.55M 15s
42400K .......... .......... .......... .......... .......... 15% 13.0M 15s
42450K .......... .......... .......... .......... .......... 15% 16.5M 15s
42500K .......... .......... .......... .......... .......... 16% 13.0M 15s
42550K .......... .......... .......... .......... .......... 16% 8.89M 15s
42600K .......... .......... .......... .......... .......... 16% 8.66M 15s
42650K .......... .......... .......... .......... .......... 16% 15.9M 15s
42700K .......... .......... .......... .......... .......... 16% 10.2M 15s
42750K .......... .......... .......... .......... .......... 16% 10.5M 15s
42800K .......... .......... .......... .......... .......... 16% 23.2M 15s
42850K .......... .......... .......... .......... .......... 16% 9.97M 15s
42900K .......... .......... .......... .......... .......... 16% 14.0M 15s
42950K .......... .......... .......... .......... .......... 16% 7.82M 15s
43000K .......... .......... .......... .......... .......... 16% 16.6M 15s
43050K .......... .......... .......... .......... .......... 16% 8.57M 15s
43100K .......... .......... .......... .......... .......... 16% 7.99M 15s
43150K .......... .......... .......... .......... .......... 16% 20.4M 15s
43200K .......... .......... .......... .......... .......... 16% 9.59M 15s
43250K .......... .......... .......... .......... .......... 16% 10.6M 15s
43300K .......... .......... .......... .......... .......... 16% 17.5M 15s
43350K .......... .......... .......... .......... .......... 16% 9.79M 15s
43400K .......... .......... .......... .......... .......... 16% 13.4M 15s
43450K .......... .......... .......... .......... .......... 16% 11.7M 15s
43500K .......... .......... .......... .......... .......... 16% 12.3M 15s
43550K .......... .......... .......... .......... .......... 16% 9.52M 15s
43600K .......... .......... .......... .......... .......... 16% 11.6M 15s
43650K .......... .......... .......... .......... .......... 16% 10.8M 15s
43700K .......... .......... .......... .......... .......... 16% 12.1M 15s
43750K .......... .......... .......... .......... .......... 16% 13.7M 15s
43800K .......... .......... .......... .......... .......... 16% 15.4M 15s
43850K .......... .......... .......... .......... .......... 16% 9.10M 15s
43900K .......... .......... .......... .......... .......... 16% 17.2M 15s
43950K .......... .......... .......... .......... .......... 16% 12.9M 15s
44000K .......... .......... .......... .......... .......... 16% 10.1M 15s
44050K .......... .......... .......... .......... .......... 16% 14.5M 15s
44100K .......... .......... .......... .......... .......... 16% 12.5M 15s
44150K .......... .......... .......... .......... .......... 16% 11.6M 15s
44200K .......... .......... .......... .......... .......... 16% 9.11M 15s
44250K .......... .......... .......... .......... .......... 16% 21.1M 15s
44300K .......... .......... .......... .......... .......... 16% 10.3M 15s
44350K .......... .......... .......... .......... .......... 16% 8.36M 15s
44400K .......... .......... .......... .......... .......... 16% 11.1M 15s
44450K .......... .......... .......... .......... .......... 16% 11.4M 15s
44500K .......... .......... .......... .......... .......... 16% 14.7M 15s
44550K .......... .......... .......... .......... .......... 16% 7.26M 15s
44600K .......... .......... .......... .......... .......... 16% 10.1M 15s
44650K .......... .......... .......... .......... .......... 16% 13.2M 15s
44700K .......... .......... .......... .......... .......... 16% 8.52M 15s
44750K .......... .......... .......... .......... .......... 16% 8.51M 15s
44800K .......... .......... .......... .......... .......... 16% 10.4M 15s
44850K .......... .......... .......... .......... .......... 16% 7.67M 15s
44900K .......... .......... .......... .......... .......... 16% 11.8M 15s
44950K .......... .......... .......... .......... .......... 16% 7.78M 15s
45000K .......... .......... .......... .......... .......... 16% 8.90M 15s
45050K .......... .......... .......... .......... .......... 16% 18.6M 15s
45100K .......... .......... .......... .......... .......... 16% 10.9M 15s
45150K .......... .......... .......... .......... .......... 17% 12.3M 15s
45200K .......... .......... .......... .......... .......... 17% 10.2M 15s
45250K .......... .......... .......... .......... .......... 17% 9.88M 15s
45300K .......... .......... .......... .......... .......... 17% 18.5M 15s
45350K .......... .......... .......... .......... .......... 17% 9.36M 15s
45400K .......... .......... .......... .......... .......... 17% 10.7M 15s
45450K .......... .......... .......... .......... .......... 17% 17.4M 15s
45500K .......... .......... .......... .......... .......... 17% 10.5M 15s
45550K .......... .......... .......... .......... .......... 17% 16.6M 15s
45600K .......... .......... .......... .......... .......... 17% 7.86M 15s
45650K .......... .......... .......... .......... .......... 17% 17.9M 15s
45700K .......... .......... .......... .......... .......... 17% 9.43M 15s
45750K .......... .......... .......... .......... .......... 17% 10.2M 15s
45800K .......... .......... .......... .......... .......... 17% 14.2M 15s
45850K .......... .......... .......... .......... .......... 17% 11.6M 15s
45900K .......... .......... .......... .......... .......... 17% 9.36M 15s
45950K .......... .......... .......... .......... .......... 17% 13.0M 15s
46000K .......... .......... .......... .......... .......... 17% 13.8M 15s
46050K .......... .......... .......... .......... .......... 17% 11.3M 15s
46100K .......... .......... .......... .......... .......... 17% 10.2M 15s
46150K .......... .......... .......... .......... .......... 17% 14.8M 15s
46200K .......... .......... .......... .......... .......... 17% 10.6M 15s
46250K .......... .......... .......... .......... .......... 17% 9.87M 15s
46300K .......... .......... .......... .......... .......... 17% 14.3M 15s
46350K .......... .......... .......... .......... .......... 17% 9.71M 15s
46400K .......... .......... .......... .......... .......... 17% 14.3M 15s
46450K .......... .......... .......... .......... .......... 17% 9.95M 15s
46500K .......... .......... .......... .......... .......... 17% 14.3M 15s
46550K .......... .......... .......... .......... .......... 17% 16.1M 15s
46600K .......... .......... .......... .......... .......... 17% 10.0M 15s
46650K .......... .......... .......... .......... .......... 17% 10.1M 15s
46700K .......... .......... .......... .......... .......... 17% 11.3M 15s
46750K .......... .......... .......... .......... .......... 17% 10.3M 15s
46800K .......... .......... .......... .......... .......... 17% 13.7M 15s
46850K .......... .......... .......... .......... .......... 17% 12.6M 15s
46900K .......... .......... .......... .......... .......... 17% 17.0M 15s
46950K .......... .......... .......... .......... .......... 17% 6.56M 15s
47000K .......... .......... .......... .......... .......... 17% 16.4M 15s
47050K .......... .......... .......... .......... .......... 17% 33.7M 15s
47100K .......... .......... .......... .......... .......... 17% 5.92M 15s
47150K .......... .......... .......... .......... .......... 17% 13.6M 15s
47200K .......... .......... .......... .......... .......... 17% 18.9M 15s
47250K .......... .......... .......... .......... .......... 17% 18.1M 15s
47300K .......... .......... .......... .......... .......... 17% 6.65M 15s
47350K .......... .......... .......... .......... .......... 17% 15.6M 15s
47400K .......... .......... .......... .......... .......... 17% 19.1M 15s
47450K .......... .......... .......... .......... .......... 17% 8.74M 15s
47500K .......... .......... .......... .......... .......... 17% 8.98M 15s
47550K .......... .......... .......... .......... .......... 17% 23.1M 15s
47600K .......... .......... .......... .......... .......... 17% 15.0M 15s
47650K .......... .......... .......... .......... .......... 17% 6.84M 15s
47700K .......... .......... .......... .......... .......... 17% 15.0M 15s
47750K .......... .......... .......... .......... .......... 17% 17.7M 15s
47800K .......... .......... .......... .......... .......... 18% 12.7M 15s
47850K .......... .......... .......... .......... .......... 18% 6.68M 15s
47900K .......... .......... .......... .......... .......... 18% 22.0M 15s
47950K .......... .......... .......... .......... .......... 18% 12.7M 15s
48000K .......... .......... .......... .......... .......... 18% 7.07M 15s
48050K .......... .......... .......... .......... .......... 18% 16.8M 15s
48100K .......... .......... .......... .......... .......... 18% 16.9M 15s
48150K .......... .......... .......... .......... .......... 18% 13.9M 15s
48200K .......... .......... .......... .......... .......... 18% 6.58M 15s
48250K .......... .......... .......... .......... .......... 18% 24.3M 15s
48300K .......... .......... .......... .......... .......... 18% 16.8M 15s
48350K .......... .......... .......... .......... .......... 18% 6.10M 15s
48400K .......... .......... .......... .......... .......... 18% 15.9M 15s
48450K .......... .......... .......... .......... .......... 18% 18.7M 15s
48500K .......... .......... .......... .......... .......... 18% 13.7M 15s
48550K .......... .......... .......... .......... .......... 18% 7.47M 15s
48600K .......... .......... .......... .......... .......... 18% 14.8M 15s
48650K .......... .......... .......... .......... .......... 18% 18.5M 15s
48700K .......... .......... .......... .......... .......... 18% 8.41M 15s
48750K .......... .......... .......... .......... .......... 18% 8.69M 15s
48800K .......... .......... .......... .......... .......... 18% 30.1M 15s
48850K .......... .......... .......... .......... .......... 18% 13.5M 15s
48900K .......... .......... .......... .......... .......... 18% 7.24M 15s
48950K .......... .......... .......... .......... .......... 18% 13.8M 15s
49000K .......... .......... .......... .......... .......... 18% 14.3M 15s
49050K .......... .......... .......... .......... .......... 18% 12.9M 15s
49100K .......... .......... .......... .......... .......... 18% 6.69M 15s
49150K .......... .......... .......... .......... .......... 18% 25.8M 15s
49200K .......... .......... .......... .......... .......... 18% 13.6M 15s
49250K .......... .......... .......... .......... .......... 18% 10.1M 15s
49300K .......... .......... .......... .......... .......... 18% 9.41M 15s
49350K .......... .......... .......... .......... .......... 18% 12.4M 15s
49400K .......... .......... .......... .......... .......... 18% 17.7M 15s
49450K .......... .......... .......... .......... .......... 18% 6.03M 15s
49500K .......... .......... .......... .......... .......... 18% 39.8M 15s
49550K .......... .......... .......... .......... .......... 18% 14.5M 15s
49600K .......... .......... .......... .......... .......... 18% 7.93M 15s
49650K .......... .......... .......... .......... .......... 18% 10.4M 15s
49700K .......... .......... .......... .......... .......... 18% 14.8M 15s
49750K .......... .......... .......... .......... .......... 18% 13.2M 15s
49800K .......... .......... .......... .......... .......... 18% 12.2M 15s
49850K .......... .......... .......... .......... .......... 18% 9.12M 15s
49900K .......... .......... .......... .......... .......... 18% 14.2M 15s
49950K .......... .......... .......... .......... .......... 18% 15.3M 15s
50000K .......... .......... .......... .......... .......... 18% 8.83M 15s
50050K .......... .......... .......... .......... .......... 18% 11.1M 15s
50100K .......... .......... .......... .......... .......... 18% 16.5M 15s
50150K .......... .......... .......... .......... .......... 18% 14.0M 15s
50200K .......... .......... .......... .......... .......... 18% 6.68M 15s
50250K .......... .......... .......... .......... .......... 18% 21.6M 15s
50300K .......... .......... .......... .......... .......... 18% 21.0M 15s
50350K .......... .......... .......... .......... .......... 18% 9.69M 15s
50400K .......... .......... .......... .......... .......... 18% 7.64M 15s
50450K .......... .......... .......... .......... .......... 19% 13.0M 15s
50500K .......... .......... .......... .......... .......... 19% 14.6M 15s
50550K .......... .......... .......... .......... .......... 19% 17.2M 15s
50600K .......... .......... .......... .......... .......... 19% 7.28M 15s
50650K .......... .......... .......... .......... .......... 19% 13.2M 15s
50700K .......... .......... .......... .......... .......... 19% 14.0M 15s
50750K .......... .......... .......... .......... .......... 19% 15.1M 15s
50800K .......... .......... .......... .......... .......... 19% 8.86M 15s
50850K .......... .......... .......... .......... .......... 19% 12.7M 15s
50900K .......... .......... .......... .......... .......... 19% 12.9M 15s
50950K .......... .......... .......... .......... .......... 19% 6.70M 15s
51000K .......... .......... .......... .......... .......... 19% 21.6M 15s
51050K .......... .......... .......... .......... .......... 19% 19.2M 15s
51100K .......... .......... .......... .......... .......... 19% 9.76M 15s
51150K .......... .......... .......... .......... .......... 19% 8.00M 15s
51200K .......... .......... .......... .......... .......... 19% 17.7M 15s
51250K .......... .......... .......... .......... .......... 19% 16.5M 15s
51300K .......... .......... .......... .......... .......... 19% 10.1M 15s
51350K .......... .......... .......... .......... .......... 19% 8.41M 15s
51400K .......... .......... .......... .......... .......... 19% 21.3M 15s
51450K .......... .......... .......... .......... .......... 19% 10.7M 15s
51500K .......... .......... .......... .......... .......... 19% 13.6M 15s
51550K .......... .......... .......... .......... .......... 19% 8.63M 15s
51600K .......... .......... .......... .......... .......... 19% 11.1M 15s
51650K .......... .......... .......... .......... .......... 19% 18.4M 15s
51700K .......... .......... .......... .......... .......... 19% 9.83M 15s
51750K .......... .......... .......... .......... .......... 19% 10.0M 15s
51800K .......... .......... .......... .......... .......... 19% 11.8M 15s
51850K .......... .......... .......... .......... .......... 19% 13.8M 15s
51900K .......... .......... .......... .......... .......... 19% 9.11M 15s
51950K .......... .......... .......... .......... .......... 19% 10.5M 15s
52000K .......... .......... .......... .......... .......... 19% 19.1M 15s
52050K .......... .......... .......... .......... .......... 19% 13.8M 15s
52100K .......... .......... .......... .......... .......... 19% 6.11M 15s
52150K .......... .......... .......... .......... .......... 19% 20.0M 15s
52200K .......... .......... .......... .......... .......... 19% 14.7M 15s
52250K .......... .......... .......... .......... .......... 19% 15.9M 15s
52300K .......... .......... .......... .......... .......... 19% 6.58M 15s
52350K .......... .......... .......... .......... .......... 19% 10.9M 15s
52400K .......... .......... .......... .......... .......... 19% 41.6M 15s
52450K .......... .......... .......... .......... .......... 19% 14.3M 15s
52500K .......... .......... .......... .......... .......... 19% 6.56M 15s
52550K .......... .......... .......... .......... .......... 19% 11.5M 15s
52600K .......... .......... .......... .......... .......... 19% 16.7M 15s
52650K .......... .......... .......... .......... .......... 19% 14.7M 15s
52700K .......... .......... .......... .......... .......... 19% 8.19M 15s
52750K .......... .......... .......... .......... .......... 19% 10.9M 15s
52800K .......... .......... .......... .......... .......... 19% 21.6M 15s
52850K .......... .......... .......... .......... .......... 19% 8.29M 15s
52900K .......... .......... .......... .......... .......... 19% 10.9M 15s
52950K .......... .......... .......... .......... .......... 19% 11.5M 15s
53000K .......... .......... .......... .......... .......... 19% 21.8M 15s
53050K .......... .......... .......... .......... .......... 19% 8.25M 15s
53100K .......... .......... .......... .......... .......... 20% 8.03M 15s
53150K .......... .......... .......... .......... .......... 20% 18.7M 15s
53200K .......... .......... .......... .......... .......... 20% 13.6M 15s
53250K .......... .......... .......... .......... .......... 20% 10.7M 15s
53300K .......... .......... .......... .......... .......... 20% 8.43M 15s
53350K .......... .......... .......... .......... .......... 20% 14.3M 15s
53400K .......... .......... .......... .......... .......... 20% 16.4M 15s
53450K .......... .......... .......... .......... .......... 20% 10.3M 15s
53500K .......... .......... .......... .......... .......... 20% 8.55M 15s
53550K .......... .......... .......... .......... .......... 20% 13.3M 15s
53600K .......... .......... .......... .......... .......... 20% 16.6M 15s
53650K .......... .......... .......... .......... .......... 20% 9.94M 15s
53700K .......... .......... .......... .......... .......... 20% 6.20M 15s
53750K .......... .......... .......... .......... .......... 20% 37.8M 15s
53800K .......... .......... .......... .......... .......... 20% 18.7M 15s
53850K .......... .......... .......... .......... .......... 20% 9.10M 15s
53900K .......... .......... .......... .......... .......... 20% 16.2M 15s
53950K .......... .......... .......... .......... .......... 20% 8.70M 15s
54000K .......... .......... .......... .......... .......... 20% 16.6M 15s
54050K .......... .......... .......... .......... .......... 20% 10.4M 15s
54100K .......... .......... .......... .......... .......... 20% 12.1M 15s
54150K .......... .......... .......... .......... .......... 20% 8.75M 15s
54200K .......... .......... .......... .......... .......... 20% 16.8M 15s
54250K .......... .......... .......... .......... .......... 20% 10.8M 15s
54300K .......... .......... .......... .......... .......... 20% 13.6M 15s
54350K .......... .......... .......... .......... .......... 20% 7.79M 15s
54400K .......... .......... .......... .......... .......... 20% 31.5M 15s
54450K .......... .......... .......... .......... .......... 20% 8.38M 15s
54500K .......... .......... .......... .......... .......... 20% 14.4M 15s
54550K .......... .......... .......... .......... .......... 20% 9.06M 15s
54600K .......... .......... .......... .......... .......... 20% 18.2M 15s
54650K .......... .......... .......... .......... .......... 20% 8.81M 15s
54700K .......... .......... .......... .......... .......... 20% 14.0M 15s
54750K .......... .......... .......... .......... .......... 20% 8.87M 15s
54800K .......... .......... .......... .......... .......... 20% 17.3M 15s
54850K .......... .......... .......... .......... .......... 20% 9.16M 15s
54900K .......... .......... .......... .......... .......... 20% 12.3M 15s
54950K .......... .......... .......... .......... .......... 20% 9.78M 15s
55000K .......... .......... .......... .......... .......... 20% 18.6M 15s
55050K .......... .......... .......... .......... .......... 20% 8.54M 15s
55100K .......... .......... .......... .......... .......... 20% 13.9M 15s
55150K .......... .......... .......... .......... .......... 20% 8.76M 15s
55200K .......... .......... .......... .......... .......... 20% 17.9M 15s
55250K .......... .......... .......... .......... .......... 20% 8.57M 15s
55300K .......... .......... .......... .......... .......... 20% 22.2M 15s
55350K .......... .......... .......... .......... .......... 20% 7.15M 15s
55400K .......... .......... .......... .......... .......... 20% 23.4M 15s
55450K .......... .......... .......... .......... .......... 20% 8.92M 15s
55500K .......... .......... .......... .......... .......... 20% 20.9M 15s
55550K .......... .......... .......... .......... .......... 20% 6.09M 15s
55600K .......... .......... .......... .......... .......... 20% 27.8M 15s
55650K .......... .......... .......... .......... .......... 20% 12.6M 15s
55700K .......... .......... .......... .......... .......... 20% 12.6M 15s
55750K .......... .......... .......... .......... .......... 20% 6.11M 15s
55800K .......... .......... .......... .......... .......... 21% 30.3M 15s
55850K .......... .......... .......... .......... .......... 21% 11.4M 15s
55900K .......... .......... .......... .......... .......... 21% 13.8M 15s
55950K .......... .......... .......... .......... .......... 21% 5.96M 15s
56000K .......... .......... .......... .......... .......... 21% 41.6M 15s
56050K .......... .......... .......... .......... .......... 21% 9.78M 15s
56100K .......... .......... .......... .......... .......... 21% 13.1M 15s
56150K .......... .......... .......... .......... .......... 21% 21.7M 15s
56200K .......... .......... .......... .......... .......... 21% 7.19M 15s
56250K .......... .......... .......... .......... .......... 21% 20.2M 15s
56300K .......... .......... .......... .......... .......... 21% 8.59M 15s
56350K .......... .......... .......... .......... .......... 21% 8.60M 15s
56400K .......... .......... .......... .......... .......... 21% 14.6M 15s
56450K .......... .......... .......... .......... .......... 21% 14.8M 15s
56500K .......... .......... .......... .......... .......... 21% 9.39M 15s
56550K .......... .......... .......... .......... .......... 21% 19.6M 15s
56600K .......... .......... .......... .......... .......... 21% 7.02M 15s
56650K .......... .......... .......... .......... .......... 21% 20.5M 15s
56700K .......... .......... .......... .......... .......... 21% 8.75M 15s
56750K .......... .......... .......... .......... .......... 21% 17.5M 15s
56800K .......... .......... .......... .......... .......... 21% 7.05M 15s
56850K .......... .......... .......... .......... .......... 21% 18.2M 15s
56900K .......... .......... .......... .......... .......... 21% 10.9M 15s
56950K .......... .......... .......... .......... .......... 21% 18.2M 15s
57000K .......... .......... .......... .......... .......... 21% 6.42M 15s
57050K .......... .......... .......... .......... .......... 21% 18.1M 15s
57100K .......... .......... .......... .......... .......... 21% 10.5M 15s
57150K .......... .......... .......... .......... .......... 21% 31.5M 15s
57200K .......... .......... .......... .......... .......... 21% 5.56M 15s
57250K .......... .......... .......... .......... .......... 21% 20.5M 15s
57300K .......... .......... .......... .......... .......... 21% 26.4M 15s
57350K .......... .......... .......... .......... .......... 21% 10.2M 15s
57400K .......... .......... .......... .......... .......... 21% 7.56M 15s
57450K .......... .......... .......... .......... .......... 21% 14.7M 15s
57500K .......... .......... .......... .......... .......... 21% 15.0M 15s
57550K .......... .......... .......... .......... .......... 21% 13.3M 15s
57600K .......... .......... .......... .......... .......... 21% 12.2M 15s
57650K .......... .......... .......... .......... .......... 21% 7.62M 15s
57700K .......... .......... .......... .......... .......... 21% 15.7M 15s
57750K .......... .......... .......... .......... .......... 21% 13.4M 15s
57800K .......... .......... .......... .......... .......... 21% 13.0M 15s
57850K .......... .......... .......... .......... .......... 21% 6.03M 15s
57900K .......... .......... .......... .......... .......... 21% 27.0M 15s
57950K .......... .......... .......... .......... .......... 21% 16.2M 15s
58000K .......... .......... .......... .......... .......... 21% 10.9M 15s
58050K .......... .......... .......... .......... .......... 21% 9.48M 15s
58100K .......... .......... .......... .......... .......... 21% 14.5M 15s
58150K .......... .......... .......... .......... .......... 21% 16.8M 15s
58200K .......... .......... .......... .......... .......... 21% 9.92M 15s
58250K .......... .......... .......... .......... .......... 21% 15.5M 15s
58300K .......... .......... .......... .......... .......... 21% 7.87M 15s
58350K .......... .......... .......... .......... .......... 21% 16.2M 15s
58400K .......... .......... .......... .......... .......... 21% 14.2M 15s
58450K .......... .......... .......... .......... .......... 22% 9.45M 15s
58500K .......... .......... .......... .......... .......... 22% 8.38M 15s
58550K .......... .......... .......... .......... .......... 22% 20.5M 15s
58600K .......... .......... .......... .......... .......... 22% 11.9M 15s
58650K .......... .......... .......... .......... .......... 22% 17.8M 15s
58700K .......... .......... .......... .......... .......... 22% 6.36M 15s
58750K .......... .......... .......... .......... .......... 22% 29.5M 15s
58800K .......... .......... .......... .......... .......... 22% 14.5M 15s
58850K .......... .......... .......... .......... .......... 22% 10.4M 15s
58900K .......... .......... .......... .......... .......... 22% 13.6M 15s
58950K .......... .......... .......... .......... .......... 22% 8.11M 15s
59000K .......... .......... .......... .......... .......... 22% 13.3M 15s
59050K .......... .......... .......... .......... .......... 22% 15.0M 15s
59100K .......... .......... .......... .......... .......... 22% 10.3M 15s
59150K .......... .......... .......... .......... .......... 22% 8.19M 15s
59200K .......... .......... .......... .......... .......... 22% 15.1M 15s
59250K .......... .......... .......... .......... .......... 22% 14.8M 15s
59300K .......... .......... .......... .......... .......... 22% 22.2M 15s
59350K .......... .......... .......... .......... .......... 22% 5.93M 15s
59400K .......... .......... .......... .......... .......... 22% 29.4M 15s
59450K .......... .......... .......... .......... .......... 22% 9.91M 15s
59500K .......... .......... .......... .......... .......... 22% 15.9M 15s
59550K .......... .......... .......... .......... .......... 22% 13.2M 15s
59600K .......... .......... .......... .......... .......... 22% 7.57M 15s
59650K .......... .......... .......... .......... .......... 22% 18.2M 15s
59700K .......... .......... .......... .......... .......... 22% 13.1M 15s
59750K .......... .......... .......... .......... .......... 22% 13.2M 15s
59800K .......... .......... .......... .......... .......... 22% 7.28M 15s
59850K .......... .......... .......... .......... .......... 22% 20.1M 15s
59900K .......... .......... .......... .......... .......... 22% 11.2M 15s
59950K .......... .......... .......... .......... .......... 22% 11.0M 15s
60000K .......... .......... .......... .......... .......... 22% 8.72M 15s
60050K .......... .......... .......... .......... .......... 22% 13.8M 15s
60100K .......... .......... .......... .......... .......... 22% 17.5M 15s
60150K .......... .......... .......... .......... .......... 22% 14.0M 15s
60200K .......... .......... .......... .......... .......... 22% 10.1M 15s
60250K .......... .......... .......... .......... .......... 22% 7.41M 15s
60300K .......... .......... .......... .......... .......... 22% 42.5M 15s
60350K .......... .......... .......... .......... .......... 22% 10.9M 15s
60400K .......... .......... .......... .......... .......... 22% 15.1M 15s
60450K .......... .......... .......... .......... .......... 22% 5.23M 15s
60500K .......... .......... .......... .......... .......... 22% 69.3M 15s
60550K .......... .......... .......... .......... .......... 22% 16.8M 15s
60600K .......... .......... .......... .......... .......... 22% 10.8M 15s
60650K .......... .......... .......... .......... .......... 22% 6.49M 15s
60700K .......... .......... .......... .......... .......... 22% 13.7M 15s
60750K .......... .......... .......... .......... .......... 22% 28.7M 15s
60800K .......... .......... .......... .......... .......... 22% 11.5M 15s
60850K .......... .......... .......... .......... .......... 22% 12.8M 15s
60900K .......... .......... .......... .......... .......... 22% 6.21M 15s
60950K .......... .......... .......... .......... .......... 22% 64.1M 15s
61000K .......... .......... .......... .......... .......... 22% 16.6M 15s
61050K .......... .......... .......... .......... .......... 22% 12.8M 15s
61100K .......... .......... .......... .......... .......... 23% 5.53M 15s
61150K .......... .......... .......... .......... .......... 23% 24.9M 15s
61200K .......... .......... .......... .......... .......... 23% 24.2M 15s
61250K .......... .......... .......... .......... .......... 23% 11.7M 15s
61300K .......... .......... .......... .......... .......... 23% 10.5M 15s
61350K .......... .......... .......... .......... .......... 23% 7.95M 15s
61400K .......... .......... .......... .......... .......... 23% 17.0M 15s
61450K .......... .......... .......... .......... .......... 23% 11.4M 15s
61500K .......... .......... .......... .......... .......... 23% 14.2M 15s
61550K .......... .......... .......... .......... .......... 23% 7.66M 15s
61600K .......... .......... .......... .......... .......... 23% 19.2M 15s
61650K .......... .......... .......... .......... .......... 23% 19.7M 15s
61700K .......... .......... .......... .......... .......... 23% 14.1M 15s
61750K .......... .......... .......... .......... .......... 23% 5.94M 15s
61800K .......... .......... .......... .......... .......... 23% 19.7M 15s
61850K .......... .......... .......... .......... .......... 23% 15.8M 15s
61900K .......... .......... .......... .......... .......... 23% 17.5M 15s
61950K .......... .......... .......... .......... .......... 23% 9.38M 15s
62000K .......... .......... .......... .......... .......... 23% 9.19M 15s
62050K .......... .......... .......... .......... .......... 23% 14.6M 15s
62100K .......... .......... .......... .......... .......... 23% 12.7M 15s
62150K .......... .......... .......... .......... .......... 23% 18.9M 15s
62200K .......... .......... .......... .......... .......... 23% 5.49M 15s
62250K .......... .......... .......... .......... .......... 23% 22.0M 15s
62300K .......... .......... .......... .......... .......... 23% 28.4M 15s
62350K .......... .......... .......... .......... .......... 23% 14.5M 15s
62400K .......... .......... .......... .......... .......... 23% 12.4M 15s
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62700K .......... .......... .......... .......... .......... 23% 7.77M 15s
62750K .......... .......... .......... .......... .......... 23% 18.4M 15s
62800K .......... .......... .......... .......... .......... 23% 20.8M 15s
62850K .......... .......... .......... .......... .......... 23% 13.3M 15s
62900K .......... .......... .......... .......... .......... 23% 6.23M 15s
62950K .......... .......... .......... .......... .......... 23% 14.2M 15s
63000K .......... .......... .......... .......... .......... 23% 17.0M 15s
63050K .......... .......... .......... .......... .......... 23% 15.9M 15s
63100K .......... .......... .......... .......... .......... 23% 9.07M 15s
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63200K .......... .......... .......... .......... .......... 23% 14.0M 15s
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63400K .......... .......... .......... .......... .......... 23% 15.0M 15s
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63600K .......... .......... .......... .......... .......... 23% 6.67M 15s
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63700K .......... .......... .......... .......... .......... 23% 11.0M 15s
63750K .......... .......... .......... .......... .......... 24% 19.3M 15s
63800K .......... .......... .......... .......... .......... 24% 9.26M 15s
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64000K .......... .......... .......... .......... .......... 24% 13.5M 15s
64050K .......... .......... .......... .......... .......... 24% 6.42M 15s
64100K .......... .......... .......... .......... .......... 24% 14.4M 15s
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64200K .......... .......... .......... .......... .......... 24% 17.1M 15s
64250K .......... .......... .......... .......... .......... 24% 19.0M 15s
64300K .......... .......... .......... .......... .......... 24% 6.11M 15s
64350K .......... .......... .......... .......... .......... 24% 13.6M 15s
64400K .......... .......... .......... .......... .......... 24% 24.2M 15s
64450K .......... .......... .......... .......... .......... 24% 16.3M 15s
64500K .......... .......... .......... .......... .......... 24% 8.05M 15s
64550K .......... .......... .......... .......... .......... 24% 9.86M 15s
64600K .......... .......... .......... .......... .......... 24% 14.7M 15s
64650K .......... .......... .......... .......... .......... 24% 16.8M 15s
64700K .......... .......... .......... .......... .......... 24% 15.1M 15s
64750K .......... .......... .......... .......... .......... 24% 9.07M 15s
64800K .......... .......... .......... .......... .......... 24% 7.93M 15s
64850K .......... .......... .......... .......... .......... 24% 24.2M 15s
64900K .......... .......... .......... .......... .......... 24% 10.7M 15s
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65000K .......... .......... .......... .......... .......... 24% 105M 15s
65050K .......... .......... .......... .......... .......... 24% 37.9M 15s
65100K .......... .......... .......... .......... .......... 24% 25.6M 15s
65150K .......... .......... .......... .......... .......... 24% 57.5M 15s
65200K .......... .......... .......... .......... .......... 24% 47.3M 15s
65250K .......... .......... .......... .......... .......... 24% 2.76M 15s
65300K .......... .......... .......... .......... .......... 24% 53.6M 15s
65350K .......... .......... .......... .......... .......... 24% 83.9M 15s
65400K .......... .......... .......... .......... .......... 24% 50.4M 15s
65450K .......... .......... .......... .......... .......... 24% 9.65M 15s
65500K .......... .......... .......... .......... .......... 24% 5.81M 15s
65550K .......... .......... .......... .......... .......... 24% 11.8M 15s
65600K .......... .......... .......... .......... .......... 24% 6.90M 15s
65650K .......... .......... .......... .......... .......... 24% 7.40M 15s
65700K .......... .......... .......... .......... .......... 24% 7.30M 15s
65750K .......... .......... .......... .......... .......... 24% 5.62M 15s
65800K .......... .......... .......... .......... .......... 24% 11.3M 15s
65850K .......... .......... .......... .......... .......... 24% 5.92M 15s
65900K .......... .......... .......... .......... .......... 24% 10.4M 15s
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66050K .......... .......... .......... .......... .......... 24% 12.2M 15s
66100K .......... .......... .......... .......... .......... 24% 4.35M 15s
66150K .......... .......... .......... .......... .......... 24% 11.6M 15s
66200K .......... .......... .......... .......... .......... 24% 4.68M 15s
66250K .......... .......... .......... .......... .......... 24% 21.8M 15s
66300K .......... .......... .......... .......... .......... 24% 7.80M 15s
66350K .......... .......... .......... .......... .......... 24% 5.26M 15s
66400K .......... .......... .......... .......... .......... 25% 11.5M 15s
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66500K .......... .......... .......... .......... .......... 25% 11.2M 15s
66550K .......... .......... .......... .......... .......... 25% 7.51M 15s
66600K .......... .......... .......... .......... .......... 25% 6.54M 15s
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66700K .......... .......... .......... .......... .......... 25% 5.39M 15s
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66850K .......... .......... .......... .......... .......... 25% 14.6M 15s
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67000K .......... .......... .......... .......... .......... 25% 11.7M 15s
67050K .......... .......... .......... .......... .......... 25% 4.48M 15s
67100K .......... .......... .......... .......... .......... 25% 11.9M 15s
67150K .......... .......... .......... .......... .......... 25% 7.01M 15s
67200K .......... .......... .......... .......... .......... 25% 3.11M 15s
67250K .......... .......... .......... .......... .......... 25% 1.88M 15s
67300K .......... .......... .......... .......... .......... 25% 21.7M 15s
67350K .......... .......... .......... .......... .......... 25% 80.2M 15s
67400K .......... .......... .......... .......... .......... 25% 21.4M 15s
67450K .......... .......... .......... .......... .......... 25% 6.27M 15s
67500K .......... .......... .......... .......... .......... 25% 4.15M 15s
67550K .......... .......... .......... .......... .......... 25% 6.77M 15s
67600K .......... .......... .......... .......... .......... 25% 5.08M 15s
67650K .......... .......... .......... .......... .......... 25% 6.38M 15s
67700K .......... .......... .......... .......... .......... 25% 4.33M 15s
67750K .......... .......... .......... .......... .......... 25% 5.55M 15s
67800K .......... .......... .......... .......... .......... 25% 9.42M 15s
67850K .......... .......... .......... .......... .......... 25% 5.07M 15s
67900K .......... .......... .......... .......... .......... 25% 8.00M 15s
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68000K .......... .......... .......... .......... .......... 25% 9.49M 15s
68050K .......... .......... .......... .......... .......... 25% 6.29M 15s
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68150K .......... .......... .......... .......... .......... 25% 9.86M 15s
68200K .......... .......... .......... .......... .......... 25% 5.35M 15s
68250K .......... .......... .......... .......... .......... 25% 10.8M 15s
68300K .......... .......... .......... .......... .......... 25% 5.87M 15s
68350K .......... .......... .......... .......... .......... 25% 6.63M 15s
68400K .......... .......... .......... .......... .......... 25% 7.80M 15s
68450K .......... .......... .......... .......... .......... 25% 7.39M 15s
68500K .......... .......... .......... .......... .......... 25% 6.67M 15s
68550K .......... .......... .......... .......... .......... 25% 9.06M 15s
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68650K .......... .......... .......... .......... .......... 25% 7.40M 15s
68700K .......... .......... .......... .......... .......... 25% 6.65M 15s
68750K .......... .......... .......... .......... .......... 25% 6.07M 15s
68800K .......... .......... .......... .......... .......... 25% 11.8M 15s
68850K .......... .......... .......... .......... .......... 25% 4.62M 15s
68900K .......... .......... .......... .......... .......... 25% 12.3M 15s
68950K .......... .......... .......... .......... .......... 25% 5.07M 15s
69000K .......... .......... .......... .......... .......... 25% 11.1M 15s
69050K .......... .......... .......... .......... .......... 26% 5.65M 15s
69100K .......... .......... .......... .......... .......... 26% 7.17M 15s
69150K .......... .......... .......... .......... .......... 26% 6.87M 15s
69200K .......... .......... .......... .......... .......... 26% 7.64M 15s
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69300K .......... .......... .......... .......... .......... 26% 7.75M 15s
69350K .......... .......... .......... .......... .......... 26% 5.93M 15s
69400K .......... .......... .......... .......... .......... 26% 8.93M 15s
69450K .......... .......... .......... .......... .......... 26% 5.82M 15s
69500K .......... .......... .......... .......... .......... 26% 9.56M 15s
69550K .......... .......... .......... .......... .......... 26% 6.68M 15s
69600K .......... .......... .......... .......... .......... 26% 7.88M 15s
69650K .......... .......... .......... .......... .......... 26% 6.44M 15s
69700K .......... .......... .......... .......... .......... 26% 7.32M 15s
69750K .......... .......... .......... .......... .......... 26% 7.58M 15s
69800K .......... .......... .......... .......... .......... 26% 8.59M 15s
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69900K .......... .......... .......... .......... .......... 26% 13.7M 15s
69950K .......... .......... .......... .......... .......... 26% 5.37M 15s
70000K .......... .......... .......... .......... .......... 26% 13.9M 15s
70050K .......... .......... .......... .......... .......... 26% 5.45M 15s
70100K .......... .......... .......... .......... .......... 26% 12.1M 15s
70150K .......... .......... .......... .......... .......... 26% 5.74M 15s
70200K .......... .......... .......... .......... .......... 26% 12.0M 15s
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70300K .......... .......... .......... .......... .......... 26% 13.3M 15s
70350K .......... .......... .......... .......... .......... 26% 5.31M 15s
70400K .......... .......... .......... .......... .......... 26% 17.7M 15s
70450K .......... .......... .......... .......... .......... 26% 4.94M 15s
70500K .......... .......... .......... .......... .......... 26% 17.4M 15s
70550K .......... .......... .......... .......... .......... 26% 8.57M 15s
70600K .......... .......... .......... .......... .......... 26% 8.53M 15s
70650K .......... .......... .......... .......... .......... 26% 6.63M 15s
70700K .......... .......... .......... .......... .......... 26% 8.48M 15s
70750K .......... .......... .......... .......... .......... 26% 6.90M 15s
70800K .......... .......... .......... .......... .......... 26% 8.63M 15s
70850K .......... .......... .......... .......... .......... 26% 9.12M 15s
70900K .......... .......... .......... .......... .......... 26% 7.12M 15s
70950K .......... .......... .......... .......... .......... 26% 8.27M 15s
71000K .......... .......... .......... .......... .......... 26% 7.45M 15s
71050K .......... .......... .......... .......... .......... 26% 18.5M 15s
71100K .......... .......... .......... .......... .......... 26% 4.58M 15s
71150K .......... .......... .......... .......... .......... 26% 19.4M 15s
71200K .......... .......... .......... .......... .......... 26% 6.19M 15s
71250K .......... .......... .......... .......... .......... 26% 9.45M 15s
71300K .......... .......... .......... .......... .......... 26% 13.5M 15s
71350K .......... .......... .......... .......... .......... 26% 5.15M 15s
71400K .......... .......... .......... .......... .......... 26% 13.0M 15s
71450K .......... .......... .......... .......... .......... 26% 5.97M 15s
71500K .......... .......... .......... .......... .......... 26% 13.8M 15s
71550K .......... .......... .......... .......... .......... 26% 5.88M 15s
71600K .......... .......... .......... .......... .......... 26% 11.3M 15s
71650K .......... .......... .......... .......... .......... 26% 10.0M 15s
71700K .......... .......... .......... .......... .......... 26% 6.82M 15s
71750K .......... .......... .......... .......... .......... 27% 13.6M 15s
71800K .......... .......... .......... .......... .......... 27% 8.49M 15s
71850K .......... .......... .......... .......... .......... 27% 11.0M 15s
71900K .......... .......... .......... .......... .......... 27% 5.60M 15s
71950K .......... .......... .......... .......... .......... 27% 11.9M 15s
72000K .......... .......... .......... .......... .......... 27% 7.16M 15s
72050K .......... .......... .......... .......... .......... 27% 11.3M 15s
72100K .......... .......... .......... .......... .......... 27% 10.3M 15s
72150K .......... .......... .......... .......... .......... 27% 6.40M 15s
72200K .......... .......... .......... .......... .......... 27% 10.2M 15s
72250K .......... .......... .......... .......... .......... 27% 5.93M 15s
72300K .......... .......... .......... .......... .......... 27% 15.0M 15s
72350K .......... .......... .......... .......... .......... 27% 10.8M 15s
72400K .......... .......... .......... .......... .......... 27% 6.75M 15s
72450K .......... .......... .......... .......... .......... 27% 9.71M 15s
72500K .......... .......... .......... .......... .......... 27% 7.66M 15s
72550K .......... .......... .......... .......... .......... 27% 15.1M 15s
72600K .......... .......... .......... .......... .......... 27% 5.07M 15s
72650K .......... .......... .......... .......... .......... 27% 14.6M 15s
72700K .......... .......... .......... .......... .......... 27% 8.50M 15s
72750K .......... .......... .......... .......... .......... 27% 7.27M 15s
72800K .......... .......... .......... .......... .......... 27% 10.1M 15s
72850K .......... .......... .......... .......... .......... 27% 6.81M 15s
72900K .......... .......... .......... .......... .......... 27% 8.99M 15s
72950K .......... .......... .......... .......... .......... 27% 8.78M 15s
73000K .......... .......... .......... .......... .......... 27% 8.28M 15s
73050K .......... .......... .......... .......... .......... 27% 12.4M 15s
73100K .......... .......... .......... .......... .......... 27% 6.16M 15s
73150K .......... .......... .......... .......... .......... 27% 10.3M 15s
73200K .......... .......... .......... .......... .......... 27% 10.9M 15s
73250K .......... .......... .......... .......... .......... 27% 6.03M 15s
73300K .......... .......... .......... .......... .......... 27% 16.1M 15s
73350K .......... .......... .......... .......... .......... 27% 6.14M 15s
73400K .......... .......... .......... .......... .......... 27% 8.72M 15s
73450K .......... .......... .......... .......... .......... 27% 10.9M 15s
73500K .......... .......... .......... .......... .......... 27% 6.78M 15s
73550K .......... .......... .......... .......... .......... 27% 11.9M 15s
73600K .......... .......... .......... .......... .......... 27% 6.72M 15s
73650K .......... .......... .......... .......... .......... 27% 9.86M 15s
73700K .......... .......... .......... .......... .......... 27% 10.1M 15s
73750K .......... .......... .......... .......... .......... 27% 6.76M 15s
73800K .......... .......... .......... .......... .......... 27% 10.5M 15s
73850K .......... .......... .......... .......... .......... 27% 6.65M 15s
73900K .......... .......... .......... .......... .......... 27% 14.8M 15s
73950K .......... .......... .......... .......... .......... 27% 7.11M 15s
74000K .......... .......... .......... .......... .......... 27% 7.89M 15s
74050K .......... .......... .......... .......... .......... 27% 9.47M 15s
74100K .......... .......... .......... .......... .......... 27% 7.96M 15s
74150K .......... .......... .......... .......... .......... 27% 10.7M 15s
74200K .......... .......... .......... .......... .......... 27% 8.19M 15s
74250K .......... .......... .......... .......... .......... 27% 7.70M 15s
74300K .......... .......... .......... .......... .......... 27% 9.98M 15s
74350K .......... .......... .......... .......... .......... 27% 8.45M 15s
74400K .......... .......... .......... .......... .......... 28% 8.68M 15s
74450K .......... .......... .......... .......... .......... 28% 7.86M 15s
74500K .......... .......... .......... .......... .......... 28% 8.30M 15s
74550K .......... .......... .......... .......... .......... 28% 10.4M 15s
74600K .......... .......... .......... .......... .......... 28% 7.13M 15s
74650K .......... .......... .......... .......... .......... 28% 8.89M 15s
74700K .......... .......... .......... .......... .......... 28% 7.38M 15s
74750K .......... .......... .......... .......... .......... 28% 8.00M 15s
74800K .......... .......... .......... .......... .......... 28% 11.7M 15s
74850K .......... .......... .......... .......... .......... 28% 7.68M 15s
74900K .......... .......... .......... .......... .......... 28% 7.46M 15s
74950K .......... .......... .......... .......... .......... 28% 13.5M 15s
75000K .......... .......... .......... .......... .......... 28% 7.64M 15s
75050K .......... .......... .......... .......... .......... 28% 7.49M 15s
75100K .......... .......... .......... .......... .......... 28% 13.4M 15s
75150K .......... .......... .......... .......... .......... 28% 5.94M 15s
75200K .......... .......... .......... .......... .......... 28% 10.5M 15s
75250K .......... .......... .......... .......... .......... 28% 11.4M 15s
75300K .......... .......... .......... .......... .......... 28% 6.56M 15s
75350K .......... .......... .......... .......... .......... 28% 11.0M 15s
75400K .......... .......... .......... .......... .......... 28% 8.30M 15s
75450K .......... .......... .......... .......... .......... 28% 6.58M 15s
75500K .......... .......... .......... .......... .......... 28% 14.1M 15s
75550K .......... .......... .......... .......... .......... 28% 7.45M 15s
75600K .......... .......... .......... .......... .......... 28% 7.83M 15s
75650K .......... .......... .......... .......... .......... 28% 10.6M 15s
75700K .......... .......... .......... .......... .......... 28% 6.77M 15s
75750K .......... .......... .......... .......... .......... 28% 10.8M 15s
75800K .......... .......... .......... .......... .......... 28% 13.0M 15s
75850K .......... .......... .......... .......... .......... 28% 5.65M 15s
75900K .......... .......... .......... .......... .......... 28% 12.7M 15s
75950K .......... .......... .......... .......... .......... 28% 8.10M 15s
76000K .......... .......... .......... .......... .......... 28% 6.73M 15s
76050K .......... .......... .......... .......... .......... 28% 14.0M 15s
76100K .......... .......... .......... .......... .......... 28% 7.43M 15s
76150K .......... .......... .......... .......... .......... 28% 7.11M 15s
76200K .......... .......... .......... .......... .......... 28% 11.3M 15s
76250K .......... .......... .......... .......... .......... 28% 8.00M 15s
76300K .......... .......... .......... .......... .......... 28% 7.71M 15s
76350K .......... .......... .......... .......... .......... 28% 11.7M 15s
76400K .......... .......... .......... .......... .......... 28% 6.25M 15s
76450K .......... .......... .......... .......... .......... 28% 9.16M 15s
76500K .......... .......... .......... .......... .......... 28% 10.4M 15s
76550K .......... .......... .......... .......... .......... 28% 8.39M 15s
76600K .......... .......... .......... .......... .......... 28% 8.25M 15s
76650K .......... .......... .......... .......... .......... 28% 9.11M 15s
76700K .......... .......... .......... .......... .......... 28% 6.39M 15s
76750K .......... .......... .......... .......... .......... 28% 16.2M 15s
76800K .......... .......... .......... .......... .......... 28% 8.22M 15s
76850K .......... .......... .......... .......... .......... 28% 6.59M 15s
76900K .......... .......... .......... .......... .......... 28% 13.7M 15s
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77000K .......... .......... .......... .......... .......... 28% 7.64M 15s
77050K .......... .......... .......... .......... .......... 29% 13.5M 15s
77100K .......... .......... .......... .......... .......... 29% 7.99M 15s
77150K .......... .......... .......... .......... .......... 29% 7.55M 15s
77200K .......... .......... .......... .......... .......... 29% 10.2M 15s
77250K .......... .......... .......... .......... .......... 29% 9.81M 15s
77300K .......... .......... .......... .......... .......... 29% 6.65M 15s
77350K .......... .......... .......... .......... .......... 29% 11.2M 15s
77400K .......... .......... .......... .......... .......... 29% 8.96M 15s
77450K .......... .......... .......... .......... .......... 29% 6.76M 15s
77500K .......... .......... .......... .......... .......... 29% 13.8M 15s
77550K .......... .......... .......... .......... .......... 29% 9.29M 15s
77600K .......... .......... .......... .......... .......... 29% 6.91M 15s
77650K .......... .......... .......... .......... .......... 29% 12.8M 15s
77700K .......... .......... .......... .......... .......... 29% 5.89M 15s
77750K .......... .......... .......... .......... .......... 29% 10.2M 15s
77800K .......... .......... .......... .......... .......... 29% 13.3M 15s
77850K .......... .......... .......... .......... .......... 29% 6.44M 15s
77900K .......... .......... .......... .......... .......... 29% 9.70M 15s
77950K .......... .......... .......... .......... .......... 29% 12.4M 15s
78000K .......... .......... .......... .......... .......... 29% 6.64M 15s
78050K .......... .......... .......... .......... .......... 29% 8.37M 15s
78100K .......... .......... .......... .......... .......... 29% 11.9M 15s
78150K .......... .......... .......... .......... .......... 29% 7.00M 15s
78200K .......... .......... .......... .......... .......... 29% 7.49M 15s
78250K .......... .......... .......... .......... .......... 29% 13.3M 15s
78300K .......... .......... .......... .......... .......... 29% 6.74M 15s
78350K .......... .......... .......... .......... .......... 29% 8.48M 15s
78400K .......... .......... .......... .......... .......... 29% 14.4M 15s
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78500K .......... .......... .......... .......... .......... 29% 7.27M 15s
78550K .......... .......... .......... .......... .......... 29% 16.2M 15s
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78800K .......... .......... .......... .......... .......... 29% 11.5M 15s
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78900K .......... .......... .......... .......... .......... 29% 7.05M 15s
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79000K .......... .......... .......... .......... .......... 29% 10.0M 15s
79050K .......... .......... .......... .......... .......... 29% 6.86M 15s
79100K .......... .......... .......... .......... .......... 29% 12.1M 15s
79150K .......... .......... .......... .......... .......... 29% 8.06M 15s
79200K .......... .......... .......... .......... .......... 29% 6.88M 15s
79250K .......... .......... .......... .......... .......... 29% 11.7M 15s
79300K .......... .......... .......... .......... .......... 29% 9.16M 15s
79350K .......... .......... .......... .......... .......... 29% 8.67M 15s
79400K .......... .......... .......... .......... .......... 29% 7.86M 15s
79450K .......... .......... .......... .......... .......... 29% 9.19M 15s
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79600K .......... .......... .......... .......... .......... 29% 7.71M 15s
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79700K .......... .......... .......... .......... .......... 30% 6.76M 15s
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79850K .......... .......... .......... .......... .......... 30% 6.56M 15s
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80000K .......... .......... .......... .......... .......... 30% 9.74M 15s
80050K .......... .......... .......... .......... .......... 30% 10.3M 15s
80100K .......... .......... .......... .......... .......... 30% 9.20M 15s
80150K .......... .......... .......... .......... .......... 30% 8.01M 15s
80200K .......... .......... .......... .......... .......... 30% 8.82M 15s
80250K .......... .......... .......... .......... .......... 30% 8.97M 15s
80300K .......... .......... .......... .......... .......... 30% 10.8M 15s
80350K .......... .......... .......... .......... .......... 30% 7.56M 15s
80400K .......... .......... .......... .......... .......... 30% 8.81M 15s
80450K .......... .......... .......... .......... .......... 30% 9.08M 15s
80500K .......... .......... .......... .......... .......... 30% 9.37M 15s
80550K .......... .......... .......... .......... .......... 30% 11.8M 15s
80600K .......... .......... .......... .......... .......... 30% 6.96M 15s
80650K .......... .......... .......... .......... .......... 30% 11.2M 15s
80700K .......... .......... .......... .......... .......... 30% 12.4M 15s
80750K .......... .......... .......... .......... .......... 30% 10.6M 15s
80800K .......... .......... .......... .......... .......... 30% 7.91M 15s
80850K .......... .......... .......... .......... .......... 30% 13.2M 15s
80900K .......... .......... .......... .......... .......... 30% 11.6M 15s
80950K .......... .......... .......... .......... .......... 30% 7.92M 15s
81000K .......... .......... .......... .......... .......... 30% 2.74M 15s
81050K .......... .......... .......... .......... .......... 30% 49.1M 15s
81100K .......... .......... .......... .......... .......... 30% 57.9M 15s
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81200K .......... .......... .......... .......... .......... 30% 21.8M 15s
81250K .......... .......... .......... .......... .......... 30% 12.7M 15s
81300K .......... .......... .......... .......... .......... 30% 10.2M 15s
81350K .......... .......... .......... .......... .......... 30% 8.10M 15s
81400K .......... .......... .......... .......... .......... 30% 13.9M 15s
81450K .......... .......... .......... .......... .......... 30% 9.07M 15s
81500K .......... .......... .......... .......... .......... 30% 9.81M 15s
81550K .......... .......... .......... .......... .......... 30% 15.4M 15s
81600K .......... .......... .......... .......... .......... 30% 8.57M 15s
81650K .......... .......... .......... .......... .......... 30% 10.1M 15s
81700K .......... .......... .......... .......... .......... 30% 7.42M 15s
81750K .......... .......... .......... .......... .......... 30% 12.7M 15s
81800K .......... .......... .......... .......... .......... 30% 11.1M 15s
81850K .......... .......... .......... .......... .......... 30% 8.92M 15s
81900K .......... .......... .......... .......... .......... 30% 19.4M 15s
81950K .......... .......... .......... .......... .......... 30% 6.46M 15s
82000K .......... .......... .......... .......... .......... 30% 13.7M 15s
82050K .......... .......... .......... .......... .......... 30% 8.65M 15s
82100K .......... .......... .......... .......... .......... 30% 9.64M 15s
82150K .......... .......... .......... .......... .......... 30% 9.92M 15s
82200K .......... .......... .......... .......... .......... 30% 9.52M 15s
82250K .......... .......... .......... .......... .......... 30% 18.7M 15s
82300K .......... .......... .......... .......... .......... 30% 7.16M 15s
82350K .......... .......... .......... .......... .......... 31% 11.7M 15s
82400K .......... .......... .......... .......... .......... 31% 6.94M 15s
82450K .......... .......... .......... .......... .......... 31% 12.3M 15s
82500K .......... .......... .......... .......... .......... 31% 13.6M 15s
82550K .......... .......... .......... .......... .......... 31% 7.05M 15s
82600K .......... .......... .......... .......... .......... 31% 16.8M 15s
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82700K .......... .......... .......... .......... .......... 31% 12.0M 15s
82750K .......... .......... .......... .......... .......... 31% 8.23M 15s
82800K .......... .......... .......... .......... .......... 31% 10.5M 15s
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82900K .......... .......... .......... .......... .......... 31% 10.9M 15s
82950K .......... .......... .......... .......... .......... 31% 19.2M 15s
83000K .......... .......... .......... .......... .......... 31% 11.8M 15s
83050K .......... .......... .......... .......... .......... 31% 11.9M 15s
83100K .......... .......... .......... .......... .......... 31% 10.9M 15s
83150K .......... .......... .......... .......... .......... 31% 8.67M 15s
83200K .......... .......... .......... .......... .......... 31% 14.3M 15s
83250K .......... .......... .......... .......... .......... 31% 9.64M 15s
83300K .......... .......... .......... .......... .......... 31% 13.9M 15s
83350K .......... .......... .......... .......... .......... 31% 9.73M 15s
83400K .......... .......... .......... .......... .......... 31% 12.7M 15s
83450K .......... .......... .......... .......... .......... 31% 20.6M 15s
83500K .......... .......... .......... .......... .......... 31% 12.1M 15s
83550K .......... .......... .......... .......... .......... 31% 9.65M 15s
83600K .......... .......... .......... .......... .......... 31% 12.3M 15s
83650K .......... .......... .......... .......... .......... 31% 11.5M 15s
83700K .......... .......... .......... .......... .......... 31% 23.5M 15s
83750K .......... .......... .......... .......... .......... 31% 6.78M 15s
83800K .......... .......... .......... .......... .......... 31% 28.7M 15s
83850K .......... .......... .......... .......... .......... 31% 9.31M 15s
83900K .......... .......... .......... .......... .......... 31% 10.6M 15s
83950K .......... .......... .......... .......... .......... 31% 18.2M 15s
84000K .......... .......... .......... .......... .......... 31% 8.15M 15s
84050K .......... .......... .......... .......... .......... 31% 17.8M 15s
84100K .......... .......... .......... .......... .......... 31% 10.8M 15s
84150K .......... .......... .......... .......... .......... 31% 10.7M 15s
84200K .......... .......... .......... .......... .......... 31% 15.2M 15s
84250K .......... .......... .......... .......... .......... 31% 8.25M 15s
84300K .......... .......... .......... .......... .......... 31% 14.9M 15s
84350K .......... .......... .......... .......... .......... 31% 14.9M 15s
84400K .......... .......... .......... .......... .......... 31% 9.49M 15s
84450K .......... .......... .......... .......... .......... 31% 11.8M 15s
84500K .......... .......... .......... .......... .......... 31% 12.9M 15s
84550K .......... .......... .......... .......... .......... 31% 11.3M 15s
84600K .......... .......... .......... .......... .......... 31% 11.4M 15s
84650K .......... .......... .......... .......... .......... 31% 10.3M 15s
84700K .......... .......... .......... .......... .......... 31% 11.9M 15s
84750K .......... .......... .......... .......... .......... 31% 9.47M 15s
84800K .......... .......... .......... .......... .......... 31% 9.59M 15s
84850K .......... .......... .......... .......... .......... 31% 6.89M 15s
84900K .......... .......... .......... .......... .......... 31% 6.23M 15s
84950K .......... .......... .......... .......... .......... 31% 10.7M 15s
85000K .......... .......... .......... .......... .......... 32% 10.3M 15s
85050K .......... .......... .......... .......... .......... 32% 5.85M 15s
85100K .......... .......... .......... .......... .......... 32% 9.82M 15s
85150K .......... .......... .......... .......... .......... 32% 9.47M 15s
85200K .......... .......... .......... .......... .......... 32% 7.85M 15s
85250K .......... .......... .......... .......... .......... 32% 11.7M 15s
85300K .......... .......... .......... .......... .......... 32% 6.27M 15s
85350K .......... .......... .......... .......... .......... 32% 7.98M 15s
85400K .......... .......... .......... .......... .......... 32% 13.3M 15s
85450K .......... .......... .......... .......... .......... 32% 5.87M 15s
85500K .......... .......... .......... .......... .......... 32% 10.5M 15s
85550K .......... .......... .......... .......... .......... 32% 7.18M 15s
85600K .......... .......... .......... .......... .......... 32% 9.00M 15s
85650K .......... .......... .......... .......... .......... 32% 9.99M 15s
85700K .......... .......... .......... .......... .......... 32% 7.36M 15s
85750K .......... .......... .......... .......... .......... 32% 18.4M 15s
85800K .......... .......... .......... .......... .......... 32% 13.2M 15s
85850K .......... .......... .......... .......... .......... 32% 6.55M 15s
85900K .......... .......... .......... .......... .......... 32% 21.8M 15s
85950K .......... .......... .......... .......... .......... 32% 10.7M 15s
86000K .......... .......... .......... .......... .......... 32% 7.88M 15s
86050K .......... .......... .......... .......... .......... 32% 16.8M 15s
86100K .......... .......... .......... .......... .......... 32% 8.54M 15s
86150K .......... .......... .......... .......... .......... 32% 10.5M 15s
86200K .......... .......... .......... .......... .......... 32% 12.5M 15s
86250K .......... .......... .......... .......... .......... 32% 7.46M 15s
86300K .......... .......... .......... .......... .......... 32% 23.2M 15s
86350K .......... .......... .......... .......... .......... 32% 8.86M 15s
86400K .......... .......... .......... .......... .......... 32% 8.00M 15s
86450K .......... .......... .......... .......... .......... 32% 23.4M 15s
86500K .......... .......... .......... .......... .......... 32% 10.5M 15s
86550K .......... .......... .......... .......... .......... 32% 7.29M 15s
86600K .......... .......... .......... .......... .......... 32% 15.9M 15s
86650K .......... .......... .......... .......... .......... 32% 15.8M 15s
86700K .......... .......... .......... .......... .......... 32% 6.81M 15s
86750K .......... .......... .......... .......... .......... 32% 17.6M 15s
86800K .......... .......... .......... .......... .......... 32% 15.4M 15s
86850K .......... .......... .......... .......... .......... 32% 7.16M 15s
86900K .......... .......... .......... .......... .......... 32% 15.0M 15s
86950K .......... .......... .......... .......... .......... 32% 13.0M 15s
87000K .......... .......... .......... .......... .......... 32% 8.02M 15s
87050K .......... .......... .......... .......... .......... 32% 11.8M 15s
87100K .......... .......... .......... .......... .......... 32% 9.93M 15s
87150K .......... .......... .......... .......... .......... 32% 13.4M 15s
87200K .......... .......... .......... .......... .......... 32% 8.92M 15s
87250K .......... .......... .......... .......... .......... 32% 8.39M 15s
87300K .......... .......... .......... .......... .......... 32% 18.3M 15s
87350K .......... .......... .......... .......... .......... 32% 9.56M 15s
87400K .......... .......... .......... .......... .......... 32% 7.29M 15s
87450K .......... .......... .......... .......... .......... 32% 14.9M 15s
87500K .......... .......... .......... .......... .......... 32% 15.8M 15s
87550K .......... .......... .......... .......... .......... 32% 6.99M 15s
87600K .......... .......... .......... .......... .......... 32% 14.4M 15s
87650K .......... .......... .......... .......... .......... 33% 19.3M 15s
87700K .......... .......... .......... .......... .......... 33% 6.27M 15s
87750K .......... .......... .......... .......... .......... 33% 16.9M 15s
87800K .......... .......... .......... .......... .......... 33% 15.9M 15s
87850K .......... .......... .......... .......... .......... 33% 6.66M 15s
87900K .......... .......... .......... .......... .......... 33% 16.8M 15s
87950K .......... .......... .......... .......... .......... 33% 15.1M 15s
88000K .......... .......... .......... .......... .......... 33% 6.67M 15s
88050K .......... .......... .......... .......... .......... 33% 17.1M 15s
88100K .......... .......... .......... .......... .......... 33% 15.4M 15s
88150K .......... .......... .......... .......... .......... 33% 6.61M 15s
88200K .......... .......... .......... .......... .......... 33% 14.7M 15s
88250K .......... .......... .......... .......... .......... 33% 16.9M 15s
88300K .......... .......... .......... .......... .......... 33% 6.89M 15s
88350K .......... .......... .......... .......... .......... 33% 12.4M 15s
88400K .......... .......... .......... .......... .......... 33% 19.8M 15s
88450K .......... .......... .......... .......... .......... 33% 6.63M 15s
88500K .......... .......... .......... .......... .......... 33% 14.1M 15s
88550K .......... .......... .......... .......... .......... 33% 17.0M 15s
88600K .......... .......... .......... .......... .......... 33% 6.75M 15s
88650K .......... .......... .......... .......... .......... 33% 16.3M 15s
88700K .......... .......... .......... .......... .......... 33% 15.1M 15s
88750K .......... .......... .......... .......... .......... 33% 6.72M 15s
88800K .......... .......... .......... .......... .......... 33% 12.3M 15s
88850K .......... .......... .......... .......... .......... 33% 18.9M 15s
88900K .......... .......... .......... .......... .......... 33% 6.40M 15s
88950K .......... .......... .......... .......... .......... 33% 13.1M 15s
89000K .......... .......... .......... .......... .......... 33% 18.9M 15s
89050K .......... .......... .......... .......... .......... 33% 8.95M 15s
89100K .......... .......... .......... .......... .......... 33% 10.8M 15s
89150K .......... .......... .......... .......... .......... 33% 13.9M 15s
89200K .......... .......... .......... .......... .......... 33% 9.00M 15s
89250K .......... .......... .......... .......... .......... 33% 8.01M 15s
89300K .......... .......... .......... .......... .......... 33% 59.5M 15s
89350K .......... .......... .......... .......... .......... 33% 7.08M 15s
89400K .......... .......... .......... .......... .......... 33% 9.47M 15s
89450K .......... .......... .......... .......... .......... 33% 14.2M 15s
89500K .......... .......... .......... .......... .......... 33% 15.8M 15s
89550K .......... .......... .......... .......... .......... 33% 6.65M 15s
89600K .......... .......... .......... .......... .......... 33% 18.4M 15s
89650K .......... .......... .......... .......... .......... 33% 11.8M 15s
89700K .......... .......... .......... .......... .......... 33% 6.87M 15s
89750K .......... .......... .......... .......... .......... 33% 25.7M 15s
89800K .......... .......... .......... .......... .......... 33% 10.4M 15s
89850K .......... .......... .......... .......... .......... 33% 6.96M 15s
89900K .......... .......... .......... .......... .......... 33% 28.8M 15s
89950K .......... .......... .......... .......... .......... 33% 9.27M 15s
90000K .......... .......... .......... .......... .......... 33% 7.48M 15s
90050K .......... .......... .......... .......... .......... 33% 28.9M 15s
90100K .......... .......... .......... .......... .......... 33% 9.46M 15s
90150K .......... .......... .......... .......... .......... 33% 11.3M 15s
90200K .......... .......... .......... .......... .......... 33% 10.2M 15s
90250K .......... .......... .......... .......... .......... 33% 28.8M 15s
90300K .......... .......... .......... .......... .......... 33% 10.3M 15s
90350K .......... .......... .......... .......... .......... 34% 9.09M 15s
90400K .......... .......... .......... .......... .......... 34% 15.2M 15s
90450K .......... .......... .......... .......... .......... 34% 11.0M 15s
90500K .......... .......... .......... .......... .......... 34% 8.70M 15s
90550K .......... .......... .......... .......... .......... 34% 12.7M 15s
90600K .......... .......... .......... .......... .......... 34% 10.6M 15s
90650K .......... .......... .......... .......... .......... 34% 9.75M 15s
90700K .......... .......... .......... .......... .......... 34% 11.9M 15s
90750K .......... .......... .......... .......... .......... 34% 12.7M 15s
90800K .......... .......... .......... .......... .......... 34% 12.0M 15s
90850K .......... .......... .......... .......... .......... 34% 9.87M 15s
90900K .......... .......... .......... .......... .......... 34% 10.3M 15s
90950K .......... .......... .......... .......... .......... 34% 30.5M 15s
91000K .......... .......... .......... .......... .......... 34% 9.06M 15s
91050K .......... .......... .......... .......... .......... 34% 12.0M 15s
91100K .......... .......... .......... .......... .......... 34% 10.6M 15s
91150K .......... .......... .......... .......... .......... 34% 9.49M 15s
91200K .......... .......... .......... .......... .......... 34% 10.9M 15s
91250K .......... .......... .......... .......... .......... 34% 16.1M 15s
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91450K .......... .......... .......... .......... .......... 34% 23.5M 15s
91500K .......... .......... .......... .......... .......... 34% 7.98M 15s
91550K .......... .......... .......... .......... .......... 34% 9.45M 15s
91600K .......... .......... .......... .......... .......... 34% 20.9M 15s
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91700K .......... .......... .......... .......... .......... 34% 14.1M 15s
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91800K .......... .......... .......... .......... .......... 34% 10.1M 15s
91850K .......... .......... .......... .......... .......... 34% 8.35M 15s
91900K .......... .......... .......... .......... .......... 34% 15.7M 15s
91950K .......... .......... .......... .......... .......... 34% 17.4M 15s
92000K .......... .......... .......... .......... .......... 34% 9.43M 15s
92050K .......... .......... .......... .......... .......... 34% 8.50M 15s
92100K .......... .......... .......... .......... .......... 34% 16.8M 15s
92150K .......... .......... .......... .......... .......... 34% 8.59M 15s
92200K .......... .......... .......... .......... .......... 34% 11.8M 15s
92250K .......... .......... .......... .......... .......... 34% 13.6M 15s
92300K .......... .......... .......... .......... .......... 34% 15.2M 15s
92350K .......... .......... .......... .......... .......... 34% 6.54M 15s
92400K .......... .......... .......... .......... .......... 34% 16.4M 15s
92450K .......... .......... .......... .......... .......... 34% 2.75M 15s
92500K .......... .......... .......... .......... .......... 34% 159M 15s
92550K .......... .......... .......... .......... .......... 34% 102M 15s
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92650K .......... .......... .......... .......... .......... 34% 9.09M 15s
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92800K .......... .......... .......... .......... .......... 34% 7.35M 15s
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92900K .......... .......... .......... .......... .......... 34% 5.73M 15s
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93000K .......... .......... .......... .......... .......... 35% 7.84M 15s
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93100K .......... .......... .......... .......... .......... 35% 9.63M 15s
93150K .......... .......... .......... .......... .......... 35% 7.24M 15s
93200K .......... .......... .......... .......... .......... 35% 12.1M 15s
93250K .......... .......... .......... .......... .......... 35% 8.88M 15s
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93700K .......... .......... .......... .......... .......... 35% 7.14M 15s
93750K .......... .......... .......... .......... .......... 35% 13.8M 15s
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93850K .......... .......... .......... .......... .......... 35% 6.25M 15s
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94000K .......... .......... .......... .......... .......... 35% 11.5M 15s
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94200K .......... .......... .......... .......... .......... 35% 7.79M 15s
94250K .......... .......... .......... .......... .......... 35% 11.8M 15s
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94400K .......... .......... .......... .......... .......... 35% 7.93M 15s
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94600K .......... .......... .......... .......... .......... 35% 10.1M 15s
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94700K .......... .......... .......... .......... .......... 35% 6.27M 15s
94750K .......... .......... .......... .......... .......... 35% 8.70M 15s
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94900K .......... .......... .......... .......... .......... 35% 11.0M 15s
94950K .......... .......... .......... .......... .......... 35% 8.38M 15s
95000K .......... .......... .......... .......... .......... 35% 7.39M 15s
95050K .......... .......... .......... .......... .......... 35% 6.44M 15s
95100K .......... .......... .......... .......... .......... 35% 10.9M 14s
95150K .......... .......... .......... .......... .......... 35% 9.57M 14s
95200K .......... .......... .......... .......... .......... 35% 8.19M 14s
95250K .......... .......... .......... .......... .......... 35% 7.37M 14s
95300K .......... .......... .......... .......... .......... 35% 10.1M 14s
95350K .......... .......... .......... .......... .......... 35% 7.72M 14s
95400K .......... .......... .......... .......... .......... 35% 8.26M 14s
95450K .......... .......... .......... .......... .......... 35% 7.69M 14s
95500K .......... .......... .......... .......... .......... 35% 10.5M 14s
95550K .......... .......... .......... .......... .......... 35% 9.93M 14s
95600K .......... .......... .......... .......... .......... 35% 8.33M 14s
95650K .......... .......... .......... .......... .......... 36% 6.91M 14s
95700K .......... .......... .......... .......... .......... 36% 6.96M 14s
95750K .......... .......... .......... .......... .......... 36% 21.4M 14s
95800K .......... .......... .......... .......... .......... 36% 6.28M 14s
95850K .......... .......... .......... .......... .......... 36% 8.68M 14s
95900K .......... .......... .......... .......... .......... 36% 9.85M 14s
95950K .......... .......... .......... .......... .......... 36% 9.10M 14s
96000K .......... .......... .......... .......... .......... 36% 8.80M 14s
96050K .......... .......... .......... .......... .......... 36% 8.47M 14s
96100K .......... .......... .......... .......... .......... 36% 5.57M 14s
96150K .......... .......... .......... .......... .......... 36% 24.5M 14s
96200K .......... .......... .......... .......... .......... 36% 5.83M 14s
96250K .......... .......... .......... .......... .......... 36% 8.98M 14s
96300K .......... .......... .......... .......... .......... 36% 22.5M 14s
96350K .......... .......... .......... .......... .......... 36% 6.20M 14s
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96500K .......... .......... .......... .......... .......... 36% 9.25M 14s
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96600K .......... .......... .......... .......... .......... 36% 8.01M 14s
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96700K .......... .......... .......... .......... .......... 36% 8.42M 14s
96750K .......... .......... .......... .......... .......... 36% 9.31M 14s
96800K .......... .......... .......... .......... .......... 36% 6.35M 14s
96850K .......... .......... .......... .......... .......... 36% 11.3M 14s
96900K .......... .......... .......... .......... .......... 36% 6.76M 14s
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97000K .......... .......... .......... .......... .......... 36% 13.7M 14s
97050K .......... .......... .......... .......... .......... 36% 7.53M 14s
97100K .......... .......... .......... .......... .......... 36% 8.60M 14s
97150K .......... .......... .......... .......... .......... 36% 8.40M 14s
97200K .......... .......... .......... .......... .......... 36% 7.51M 14s
97250K .......... .......... .......... .......... .......... 36% 11.2M 14s
97300K .......... .......... .......... .......... .......... 36% 10.5M 14s
97350K .......... .......... .......... .......... .......... 36% 4.87M 14s
97400K .......... .......... .......... .......... .......... 36% 36.4M 14s
97450K .......... .......... .......... .......... .......... 36% 6.46M 14s
97500K .......... .......... .......... .......... .......... 36% 7.72M 14s
97550K .......... .......... .......... .......... .......... 36% 24.3M 14s
97600K .......... .......... .......... .......... .......... 36% 6.14M 14s
97650K .......... .......... .......... .......... .......... 36% 7.80M 14s
97700K .......... .......... .......... .......... .......... 36% 14.8M 14s
97750K .......... .......... .......... .......... .......... 36% 8.27M 14s
97800K .......... .......... .......... .......... .......... 36% 6.75M 14s
97850K .......... .......... .......... .......... .......... 36% 17.9M 14s
97900K .......... .......... .......... .......... .......... 36% 7.58M 14s
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98000K .......... .......... .......... .......... .......... 36% 16.2M 14s
98050K .......... .......... .......... .......... .......... 36% 6.68M 14s
98100K .......... .......... .......... .......... .......... 36% 7.06M 14s
98150K .......... .......... .......... .......... .......... 36% 18.5M 14s
98200K .......... .......... .......... .......... .......... 36% 7.30M 14s
98250K .......... .......... .......... .......... .......... 36% 7.27M 14s
98300K .......... .......... .......... .......... .......... 37% 16.1M 14s
98350K .......... .......... .......... .......... .......... 37% 7.14M 14s
98400K .......... .......... .......... .......... .......... 37% 7.62M 14s
98450K .......... .......... .......... .......... .......... 37% 13.0M 14s
98500K .......... .......... .......... .......... .......... 37% 7.87M 14s
98550K .......... .......... .......... .......... .......... 37% 7.27M 14s
98600K .......... .......... .......... .......... .......... 37% 13.4M 14s
98650K .......... .......... .......... .......... .......... 37% 7.46M 14s
98700K .......... .......... .......... .......... .......... 37% 7.86M 14s
98750K .......... .......... .......... .......... .......... 37% 13.8M 14s
98800K .......... .......... .......... .......... .......... 37% 8.34M 14s
98850K .......... .......... .......... .......... .......... 37% 6.55M 14s
98900K .......... .......... .......... .......... .......... 37% 16.8M 14s
98950K .......... .......... .......... .......... .......... 37% 6.81M 14s
99000K .......... .......... .......... .......... .......... 37% 7.52M 14s
99050K .......... .......... .......... .......... .......... 37% 16.0M 14s
99100K .......... .......... .......... .......... .......... 37% 6.89M 14s
99150K .......... .......... .......... .......... .......... 37% 7.92M 14s
99200K .......... .......... .......... .......... .......... 37% 7.53M 14s
99250K .......... .......... .......... .......... .......... 37% 20.0M 14s
99300K .......... .......... .......... .......... .......... 37% 6.07M 14s
99350K .......... .......... .......... .......... .......... 37% 8.47M 14s
99400K .......... .......... .......... .......... .......... 37% 20.2M 14s
99450K .......... .......... .......... .......... .......... 37% 5.95M 14s
99500K .......... .......... .......... .......... .......... 37% 12.0M 14s
99550K .......... .......... .......... .......... .......... 37% 11.8M 14s
99600K .......... .......... .......... .......... .......... 37% 6.21M 14s
99650K .......... .......... .......... .......... .......... 37% 12.8M 14s
99700K .......... .......... .......... .......... .......... 37% 9.50M 14s
99750K .......... .......... .......... .......... .......... 37% 6.86M 14s
99800K .......... .......... .......... .......... .......... 37% 10.4M 14s
99850K .......... .......... .......... .......... .......... 37% 9.65M 14s
99900K .......... .......... .......... .......... .......... 37% 7.18M 14s
99950K .......... .......... .......... .......... .......... 37% 9.67M 14s
100000K .......... .......... .......... .......... .......... 37% 9.37M 14s
100050K .......... .......... .......... .......... .......... 37% 7.15M 14s
100100K .......... .......... .......... .......... .......... 37% 11.8M 14s
100150K .......... .......... .......... .......... .......... 37% 9.42M 14s
100200K .......... .......... .......... .......... .......... 37% 6.37M 14s
100250K .......... .......... .......... .......... .......... 37% 11.2M 14s
100300K .......... .......... .......... .......... .......... 37% 9.04M 14s
100350K .......... .......... .......... .......... .......... 37% 9.13M 14s
100400K .......... .......... .......... .......... .......... 37% 9.09M 14s
100450K .......... .......... .......... .......... .......... 37% 7.89M 14s
100500K .......... .......... .......... .......... .......... 37% 11.1M 14s
100550K .......... .......... .......... .......... .......... 37% 8.35M 14s
100600K .......... .......... .......... .......... .......... 37% 8.66M 14s
100650K .......... .......... .......... .......... .......... 37% 8.30M 14s
100700K .......... .......... .......... .......... .......... 37% 7.07M 14s
100750K .......... .......... .......... .......... .......... 37% 17.9M 14s
100800K .......... .......... .......... .......... .......... 37% 7.38M 14s
100850K .......... .......... .......... .......... .......... 37% 7.53M 14s
100900K .......... .......... .......... .......... .......... 37% 14.1M 14s
100950K .......... .......... .......... .......... .......... 38% 9.04M 14s
101000K .......... .......... .......... .......... .......... 38% 6.51M 14s
101050K .......... .......... .......... .......... .......... 38% 12.8M 14s
101100K .......... .......... .......... .......... .......... 38% 8.54M 14s
101150K .......... .......... .......... .......... .......... 38% 6.82M 14s
101200K .......... .......... .......... .......... .......... 38% 10.3M 14s
101250K .......... .......... .......... .......... .......... 38% 9.06M 14s
101300K .......... .......... .......... .......... .......... 38% 9.27M 14s
101350K .......... .......... .......... .......... .......... 38% 7.87M 14s
101400K .......... .......... .......... .......... .......... 38% 11.7M 14s
101450K .......... .......... .......... .......... .......... 38% 7.41M 14s
101500K .......... .......... .......... .......... .......... 38% 7.28M 14s
101550K .......... .......... .......... .......... .......... 38% 23.1M 14s
101600K .......... .......... .......... .......... .......... 38% 6.98M 14s
101650K .......... .......... .......... .......... .......... 38% 8.63M 14s
101700K .......... .......... .......... .......... .......... 38% 9.87M 14s
101750K .......... .......... .......... .......... .......... 38% 9.92M 14s
101800K .......... .......... .......... .......... .......... 38% 9.16M 14s
101850K .......... .......... .......... .......... .......... 38% 8.26M 14s
101900K .......... .......... .......... .......... .......... 38% 10.5M 14s
101950K .......... .......... .......... .......... .......... 38% 8.50M 14s
102000K .......... .......... .......... .......... .......... 38% 9.79M 14s
102050K .......... .......... .......... .......... .......... 38% 21.3M 14s
102100K .......... .......... .......... .......... .......... 38% 7.55M 14s
102150K .......... .......... .......... .......... .......... 38% 8.02M 14s
102200K .......... .......... .......... .......... .......... 38% 15.0M 14s
102250K .......... .......... .......... .......... .......... 38% 7.39M 14s
102300K .......... .......... .......... .......... .......... 38% 14.1M 14s
102350K .......... .......... .......... .......... .......... 38% 8.80M 14s
102400K .......... .......... .......... .......... .......... 38% 12.0M 14s
102450K .......... .......... .......... .......... .......... 38% 9.50M 14s
102500K .......... .......... .......... .......... .......... 38% 10.8M 14s
102550K .......... .......... .......... .......... .......... 38% 12.5M 14s
102600K .......... .......... .......... .......... .......... 38% 8.85M 14s
102650K .......... .......... .......... .......... .......... 38% 9.42M 14s
102700K .......... .......... .......... .......... .......... 38% 13.3M 14s
102750K .......... .......... .......... .......... .......... 38% 7.72M 14s
102800K .......... .......... .......... .......... .......... 38% 16.1M 14s
102850K .......... .......... .......... .......... .......... 38% 10.0M 14s
102900K .......... .......... .......... .......... .......... 38% 6.52M 14s
102950K .......... .......... .......... .......... .......... 38% 15.7M 14s
103000K .......... .......... .......... .......... .......... 38% 12.8M 14s
103050K .......... .......... .......... .......... .......... 38% 11.2M 14s
103100K .......... .......... .......... .......... .......... 38% 8.51M 14s
103150K .......... .......... .......... .......... .......... 38% 9.97M 14s
103200K .......... .......... .......... .......... .......... 38% 12.1M 14s
103250K .......... .......... .......... .......... .......... 38% 7.97M 14s
103300K .......... .......... .......... .......... .......... 38% 16.2M 14s
103350K .......... .......... .......... .......... .......... 38% 6.63M 14s
103400K .......... .......... .......... .......... .......... 38% 8.80M 14s
103450K .......... .......... .......... .......... .......... 38% 5.86M 14s
103500K .......... .......... .......... .......... .......... 38% 2.00M 14s
103550K .......... .......... .......... .......... .......... 38% 41.4M 14s
103600K .......... .......... .......... .......... .......... 39% 117M 14s
103650K .......... .......... .......... .......... .......... 39% 163M 14s
103700K .......... .......... .......... .......... .......... 39% 8.78M 14s
103750K .......... .......... .......... .......... .......... 39% 11.8M 14s
103800K .......... .......... .......... .......... .......... 39% 6.75M 14s
103850K .......... .......... .......... .......... .......... 39% 11.4M 14s
103900K .......... .......... .......... .......... .......... 39% 6.19M 14s
103950K .......... .......... .......... .......... .......... 39% 7.69M 14s
104000K .......... .......... .......... .......... .......... 39% 8.49M 14s
104050K .......... .......... .......... .......... .......... 39% 5.65M 14s
104100K .......... .......... .......... .......... .......... 39% 14.5M 14s
104150K .......... .......... .......... .......... .......... 39% 6.18M 14s
104200K .......... .......... .......... .......... .......... 39% 7.53M 14s
104250K .......... .......... .......... .......... .......... 39% 9.54M 14s
104300K .......... .......... .......... .......... .......... 39% 9.42M 14s
104350K .......... .......... .......... .......... .......... 39% 11.6M 14s
104400K .......... .......... .......... .......... .......... 39% 9.51M 14s
104450K .......... .......... .......... .......... .......... 39% 10.8M 14s
104500K .......... .......... .......... .......... .......... 39% 10.3M 14s
104550K .......... .......... .......... .......... .......... 39% 10.5M 14s
104600K .......... .......... .......... .......... .......... 39% 12.9M 14s
104650K .......... .......... .......... .......... .......... 39% 6.17M 14s
104700K .......... .......... .......... .......... .......... 39% 15.6M 14s
104750K .......... .......... .......... .......... .......... 39% 9.21M 14s
104800K .......... .......... .......... .......... .......... 39% 14.8M 14s
104850K .......... .......... .......... .......... .......... 39% 11.6M 14s
104900K .......... .......... .......... .......... .......... 39% 7.00M 14s
104950K .......... .......... .......... .......... .......... 39% 13.2M 14s
105000K .......... .......... .......... .......... .......... 39% 9.58M 14s
105050K .......... .......... .......... .......... .......... 39% 10.5M 14s
105100K .......... .......... .......... .......... .......... 39% 10.2M 14s
105150K .......... .......... .......... .......... .......... 39% 9.11M 14s
105200K .......... .......... .......... .......... .......... 39% 14.4M 14s
105250K .......... .......... .......... .......... .......... 39% 13.8M 14s
105300K .......... .......... .......... .......... .......... 39% 7.29M 14s
105350K .......... .......... .......... .......... .......... 39% 10.2M 14s
105400K .......... .......... .......... .......... .......... 39% 8.77M 14s
105450K .......... .......... .......... .......... .......... 39% 14.9M 14s
105500K .......... .......... .......... .......... .......... 39% 14.3M 14s
105550K .......... .......... .......... .......... .......... 39% 7.25M 14s
105600K .......... .......... .......... .......... .......... 39% 11.0M 14s
105650K .......... .......... .......... .......... .......... 39% 8.57M 14s
105700K .......... .......... .......... .......... .......... 39% 15.4M 14s
105750K .......... .......... .......... .......... .......... 39% 14.5M 14s
105800K .......... .......... .......... .......... .......... 39% 6.78M 14s
105850K .......... .......... .......... .......... .......... 39% 10.5M 14s
105900K .......... .......... .......... .......... .......... 39% 16.1M 14s
105950K .......... .......... .......... .......... .......... 39% 7.87M 14s
106000K .......... .......... .......... .......... .......... 39% 14.1M 14s
106050K .......... .......... .......... .......... .......... 39% 7.32M 14s
106100K .......... .......... .......... .......... .......... 39% 16.1M 14s
106150K .......... .......... .......... .......... .......... 39% 11.5M 14s
106200K .......... .......... .......... .......... .......... 39% 7.83M 14s
106250K .......... .......... .......... .......... .......... 40% 12.3M 14s
106300K .......... .......... .......... .......... .......... 40% 8.76M 14s
106350K .......... .......... .......... .......... .......... 40% 10.7M 14s
106400K .......... .......... .......... .......... .......... 40% 11.8M 14s
106450K .......... .......... .......... .......... .......... 40% 7.58M 14s
106500K .......... .......... .......... .......... .......... 40% 13.4M 14s
106550K .......... .......... .......... .......... .......... 40% 8.39M 14s
106600K .......... .......... .......... .......... .......... 40% 11.0M 14s
106650K .......... .......... .......... .......... .......... 40% 11.5M 14s
106700K .......... .......... .......... .......... .......... 40% 9.73M 14s
106750K .......... .......... .......... .......... .......... 40% 9.53M 14s
106800K .......... .......... .......... .......... .......... 40% 10.2M 14s
106850K .......... .......... .......... .......... .......... 40% 10.0M 14s
106900K .......... .......... .......... .......... .......... 40% 15.1M 14s
106950K .......... .......... .......... .......... .......... 40% 7.31M 14s
107000K .......... .......... .......... .......... .......... 40% 12.7M 14s
107050K .......... .......... .......... .......... .......... 40% 8.23M 14s
107100K .......... .......... .......... .......... .......... 40% 13.2M 14s
107150K .......... .......... .......... .......... .......... 40% 11.8M 14s
107200K .......... .......... .......... .......... .......... 40% 8.72M 14s
107250K .......... .......... .......... .......... .......... 40% 15.5M 14s
107300K .......... .......... .......... .......... .......... 40% 12.0M 14s
107350K .......... .......... .......... .......... .......... 40% 8.86M 14s
107400K .......... .......... .......... .......... .......... 40% 10.7M 14s
107450K .......... .......... .......... .......... .......... 40% 12.3M 14s
107500K .......... .......... .......... .......... .......... 40% 8.61M 14s
107550K .......... .......... .......... .......... .......... 40% 16.5M 14s
107600K .......... .......... .......... .......... .......... 40% 8.39M 14s
107650K .......... .......... .......... .......... .......... 40% 11.1M 14s
107700K .......... .......... .......... .......... .......... 40% 12.7M 14s
107750K .......... .......... .......... .......... .......... 40% 10.2M 14s
107800K .......... .......... .......... .......... .......... 40% 12.8M 14s
107850K .......... .......... .......... .......... .......... 40% 11.7M 14s
107900K .......... .......... .......... .......... .......... 40% 9.67M 14s
107950K .......... .......... .......... .......... .......... 40% 11.1M 14s
108000K .......... .......... .......... .......... .......... 40% 14.4M 14s
108050K .......... .......... .......... .......... .......... 40% 7.38M 14s
108100K .......... .......... .......... .......... .......... 40% 13.2M 14s
108150K .......... .......... .......... .......... .......... 40% 13.9M 14s
108200K .......... .......... .......... .......... .......... 40% 7.05M 14s
108250K .......... .......... .......... .......... .......... 40% 14.2M 14s
108300K .......... .......... .......... .......... .......... 40% 11.6M 14s
108350K .......... .......... .......... .......... .......... 40% 9.18M 14s
108400K .......... .......... .......... .......... .......... 40% 12.6M 14s
108450K .......... .......... .......... .......... .......... 40% 8.45M 14s
108500K .......... .......... .......... .......... .......... 40% 14.7M 14s
108550K .......... .......... .......... .......... .......... 40% 12.9M 14s
108600K .......... .......... .......... .......... .......... 40% 8.78M 14s
108650K .......... .......... .......... .......... .......... 40% 12.0M 14s
108700K .......... .......... .......... .......... .......... 40% 16.5M 14s
108750K .......... .......... .......... .......... .......... 40% 8.52M 14s
108800K .......... .......... .......... .......... .......... 40% 10.3M 14s
108850K .......... .......... .......... .......... .......... 40% 12.5M 14s
108900K .......... .......... .......... .......... .......... 40% 8.51M 14s
108950K .......... .......... .......... .......... .......... 41% 9.85M 14s
109000K .......... .......... .......... .......... .......... 41% 12.2M 14s
109050K .......... .......... .......... .......... .......... 41% 9.11M 14s
109100K .......... .......... .......... .......... .......... 41% 12.6M 14s
109150K .......... .......... .......... .......... .......... 41% 8.42M 14s
109200K .......... .......... .......... .......... .......... 41% 13.9M 14s
109250K .......... .......... .......... .......... .......... 41% 13.2M 14s
109300K .......... .......... .......... .......... .......... 41% 8.52M 14s
109350K .......... .......... .......... .......... .......... 41% 10.4M 14s
109400K .......... .......... .......... .......... .......... 41% 15.6M 14s
109450K .......... .......... .......... .......... .......... 41% 8.56M 14s
109500K .......... .......... .......... .......... .......... 41% 12.0M 14s
109550K .......... .......... .......... .......... .......... 41% 14.3M 14s
109600K .......... .......... .......... .......... .......... 41% 8.97M 14s
109650K .......... .......... .......... .......... .......... 41% 11.9M 14s
109700K .......... .......... .......... .......... .......... 41% 11.8M 14s
109750K .......... .......... .......... .......... .......... 41% 10.3M 14s
109800K .......... .......... .......... .......... .......... 41% 11.5M 14s
109850K .......... .......... .......... .......... .......... 41% 11.9M 14s
109900K .......... .......... .......... .......... .......... 41% 11.8M 14s
109950K .......... .......... .......... .......... .......... 41% 7.25M 14s
110000K .......... .......... .......... .......... .......... 41% 42.0M 14s
110050K .......... .......... .......... .......... .......... 41% 13.3M 14s
110100K .......... .......... .......... .......... .......... 41% 6.45M 14s
110150K .......... .......... .......... .......... .......... 41% 43.4M 14s
110200K .......... .......... .......... .......... .......... 41% 3.02M 14s
110250K .......... .......... .......... .......... .......... 41% 43.0M 14s
110300K .......... .......... .......... .......... .......... 41% 65.7M 14s
110350K .......... .......... .......... .......... .......... 41% 42.6M 14s
110400K .......... .......... .......... .......... .......... 41% 11.5M 14s
110450K .......... .......... .......... .......... .......... 41% 7.90M 14s
110500K .......... .......... .......... .......... .......... 41% 10.6M 14s
110550K .......... .......... .......... .......... .......... 41% 12.4M 14s
110600K .......... .......... .......... .......... .......... 41% 7.20M 14s
110650K .......... .......... .......... .......... .......... 41% 11.5M 14s
110700K .......... .......... .......... .......... .......... 41% 7.09M 14s
110750K .......... .......... .......... .......... .......... 41% 18.6M 14s
110800K .......... .......... .......... .......... .......... 41% 6.02M 14s
110850K .......... .......... .......... .......... .......... 41% 16.7M 14s
110900K .......... .......... .......... .......... .......... 41% 5.91M 14s
110950K .......... .......... .......... .......... .......... 41% 15.6M 14s
111000K .......... .......... .......... .......... .......... 41% 5.90M 14s
111050K .......... .......... .......... .......... .......... 41% 18.2M 14s
111100K .......... .......... .......... .......... .......... 41% 5.82M 14s
111150K .......... .......... .......... .......... .......... 41% 14.6M 14s
111200K .......... .......... .......... .......... .......... 41% 7.95M 14s
111250K .......... .......... .......... .......... .......... 41% 12.3M 14s
111300K .......... .......... .......... .......... .......... 41% 7.84M 14s
111350K .......... .......... .......... .......... .......... 41% 9.11M 14s
111400K .......... .......... .......... .......... .......... 41% 15.1M 14s
111450K .......... .......... .......... .......... .......... 41% 5.94M 14s
111500K .......... .......... .......... .......... .......... 41% 16.8M 14s
111550K .......... .......... .......... .......... .......... 41% 6.39M 14s
111600K .......... .......... .......... .......... .......... 42% 15.7M 14s
111650K .......... .......... .......... .......... .......... 42% 6.34M 14s
111700K .......... .......... .......... .......... .......... 42% 15.8M 14s
111750K .......... .......... .......... .......... .......... 42% 6.34M 14s
111800K .......... .......... .......... .......... .......... 42% 19.6M 13s
111850K .......... .......... .......... .......... .......... 42% 7.90M 13s
111900K .......... .......... .......... .......... .......... 42% 9.82M 13s
111950K .......... .......... .......... .......... .......... 42% 9.58M 13s
112000K .......... .......... .......... .......... .......... 42% 9.28M 13s
112050K .......... .......... .......... .......... .......... 42% 17.4M 13s
112100K .......... .......... .......... .......... .......... 42% 6.38M 13s
112150K .......... .......... .......... .......... .......... 42% 18.7M 13s
112200K .......... .......... .......... .......... .......... 42% 6.16M 13s
112250K .......... .......... .......... .......... .......... 42% 21.5M 13s
112300K .......... .......... .......... .......... .......... 42% 7.81M 13s
112350K .......... .......... .......... .......... .......... 42% 10.4M 13s
112400K .......... .......... .......... .......... .......... 42% 8.99M 13s
112450K .......... .......... .......... .......... .......... 42% 8.38M 13s
112500K .......... .......... .......... .......... .......... 42% 21.0M 13s
112550K .......... .......... .......... .......... .......... 42% 8.29M 13s
112600K .......... .......... .......... .......... .......... 42% 11.2M 13s
112650K .......... .......... .......... .......... .......... 42% 6.90M 13s
112700K .......... .......... .......... .......... .......... 42% 12.1M 13s
112750K .......... .......... .......... .......... .......... 42% 10.4M 13s
112800K .......... .......... .......... .......... .......... 42% 8.77M 13s
112850K .......... .......... .......... .......... .......... 42% 17.2M 13s
112900K .......... .......... .......... .......... .......... 42% 6.41M 13s
112950K .......... .......... .......... .......... .......... 42% 12.5M 13s
113000K .......... .......... .......... .......... .......... 42% 9.01M 13s
113050K .......... .......... .......... .......... .......... 42% 11.5M 13s
113100K .......... .......... .......... .......... .......... 42% 15.4M 13s
113150K .......... .......... .......... .......... .......... 42% 6.08M 13s
113200K .......... .......... .......... .......... .......... 42% 17.8M 13s
113250K .......... .......... .......... .......... .......... 42% 5.47M 13s
113300K .......... .......... .......... .......... .......... 42% 27.2M 13s
113350K .......... .......... .......... .......... .......... 42% 9.07M 13s
113400K .......... .......... .......... .......... .......... 42% 8.89M 13s
113450K .......... .......... .......... .......... .......... 42% 10.6M 13s
113500K .......... .......... .......... .......... .......... 42% 7.59M 13s
113550K .......... .......... .......... .......... .......... 42% 18.8M 13s
113600K .......... .......... .......... .......... .......... 42% 6.60M 13s
113650K .......... .......... .......... .......... .......... 42% 15.4M 13s
113700K .......... .......... .......... .......... .......... 42% 11.0M 13s
113750K .......... .......... .......... .......... .......... 42% 7.55M 13s
113800K .......... .......... .......... .......... .......... 42% 32.4M 13s
113850K .......... .......... .......... .......... .......... 42% 6.97M 13s
113900K .......... .......... .......... .......... .......... 42% 16.1M 13s
113950K .......... .......... .......... .......... .......... 42% 9.57M 13s
114000K .......... .......... .......... .......... .......... 42% 9.40M 13s
114050K .......... .......... .......... .......... .......... 42% 18.4M 13s
114100K .......... .......... .......... .......... .......... 42% 6.44M 13s
114150K .......... .......... .......... .......... .......... 42% 30.4M 13s
114200K .......... .......... .......... .......... .......... 42% 12.8M 13s
114250K .......... .......... .......... .......... .......... 43% 7.34M 13s
114300K .......... .......... .......... .......... .......... 43% 15.8M 13s
114350K .......... .......... .......... .......... .......... 43% 9.73M 13s
114400K .......... .......... .......... .......... .......... 43% 17.1M 13s
114450K .......... .......... .......... .......... .......... 43% 15.3M 13s
114500K .......... .......... .......... .......... .......... 43% 7.77M 13s
114550K .......... .......... .......... .......... .......... 43% 15.3M 13s
114600K .......... .......... .......... .......... .......... 43% 16.7M 13s
114650K .......... .......... .......... .......... .......... 43% 9.38M 13s
114700K .......... .......... .......... .......... .......... 43% 18.2M 13s
114750K .......... .......... .......... .......... .......... 43% 7.24M 13s
114800K .......... .......... .......... .......... .......... 43% 23.1M 13s
114850K .......... .......... .......... .......... .......... 43% 12.5M 13s
114900K .......... .......... .......... .......... .......... 43% 8.73M 13s
114950K .......... .......... .......... .......... .......... 43% 19.1M 13s
115000K .......... .......... .......... .......... .......... 43% 8.47M 13s
115050K .......... .......... .......... .......... .......... 43% 15.2M 13s
115100K .......... .......... .......... .......... .......... 43% 15.4M 13s
115150K .......... .......... .......... .......... .......... 43% 7.97M 13s
115200K .......... .......... .......... .......... .......... 43% 16.4M 13s
115250K .......... .......... .......... .......... .......... 43% 8.48M 13s
115300K .......... .......... .......... .......... .......... 43% 13.6M 13s
115350K .......... .......... .......... .......... .......... 43% 14.2M 13s
115400K .......... .......... .......... .......... .......... 43% 9.14M 13s
115450K .......... .......... .......... .......... .......... 43% 15.4M 13s
115500K .......... .......... .......... .......... .......... 43% 8.08M 13s
115550K .......... .......... .......... .......... .......... 43% 15.0M 13s
115600K .......... .......... .......... .......... .......... 43% 15.5M 13s
115650K .......... .......... .......... .......... .......... 43% 7.99M 13s
115700K .......... .......... .......... .......... .......... 43% 14.2M 13s
115750K .......... .......... .......... .......... .......... 43% 18.2M 13s
115800K .......... .......... .......... .......... .......... 43% 8.01M 13s
115850K .......... .......... .......... .......... .......... 43% 12.3M 13s
115900K .......... .......... .......... .......... .......... 43% 9.46M 13s
115950K .......... .......... .......... .......... .......... 43% 13.4M 13s
116000K .......... .......... .......... .......... .......... 43% 14.6M 13s
116050K .......... .......... .......... .......... .......... 43% 8.56M 13s
116100K .......... .......... .......... .......... .......... 43% 16.7M 13s
116150K .......... .......... .......... .......... .......... 43% 8.07M 13s
116200K .......... .......... .......... .......... .......... 43% 17.9M 13s
116250K .......... .......... .......... .......... .......... 43% 12.2M 13s
116300K .......... .......... .......... .......... .......... 43% 9.48M 13s
116350K .......... .......... .......... .......... .......... 43% 16.7M 13s
116400K .......... .......... .......... .......... .......... 43% 11.3M 13s
116450K .......... .......... .......... .......... .......... 43% 8.55M 13s
116500K .......... .......... .......... .......... .......... 43% 19.7M 13s
116550K .......... .......... .......... .......... .......... 43% 2.77M 13s
116600K .......... .......... .......... .......... .......... 43% 83.0M 13s
116650K .......... .......... .......... .......... .......... 43% 101M 13s
116700K .......... .......... .......... .......... .......... 43% 102M 13s
116750K .......... .......... .......... .......... .......... 43% 12.6M 13s
116800K .......... .......... .......... .......... .......... 43% 7.63M 13s
116850K .......... .......... .......... .......... .......... 43% 9.25M 13s
116900K .......... .......... .......... .......... .......... 44% 8.48M 13s
116950K .......... .......... .......... .......... .......... 44% 12.0M 13s
117000K .......... .......... .......... .......... .......... 44% 8.41M 13s
117050K .......... .......... .......... .......... .......... 44% 11.7M 13s
117100K .......... .......... .......... .......... .......... 44% 8.87M 13s
117150K .......... .......... .......... .......... .......... 44% 6.42M 13s
117200K .......... .......... .......... .......... .......... 44% 20.7M 13s
117250K .......... .......... .......... .......... .......... 44% 7.69M 13s
117300K .......... .......... .......... .......... .......... 44% 14.2M 13s
117350K .......... .......... .......... .......... .......... 44% 7.89M 13s
117400K .......... .......... .......... .......... .......... 44% 12.6M 13s
117450K .......... .......... .......... .......... .......... 44% 8.27M 13s
117500K .......... .......... .......... .......... .......... 44% 11.0M 13s
117550K .......... .......... .......... .......... .......... 44% 8.66M 13s
117600K .......... .......... .......... .......... .......... 44% 12.0M 13s
117650K .......... .......... .......... .......... .......... 44% 8.52M 13s
117700K .......... .......... .......... .......... .......... 44% 11.0M 13s
117750K .......... .......... .......... .......... .......... 44% 9.36M 13s
117800K .......... .......... .......... .......... .......... 44% 12.6M 13s
117850K .......... .......... .......... .......... .......... 44% 7.66M 13s
117900K .......... .......... .......... .......... .......... 44% 12.1M 13s
117950K .......... .......... .......... .......... .......... 44% 7.85M 13s
118000K .......... .......... .......... .......... .......... 44% 11.5M 13s
118050K .......... .......... .......... .......... .......... 44% 8.29M 13s
118100K .......... .......... .......... .......... .......... 44% 10.6M 13s
118150K .......... .......... .......... .......... .......... 44% 13.8M 13s
118200K .......... .......... .......... .......... .......... 44% 7.33M 13s
118250K .......... .......... .......... .......... .......... 44% 17.3M 13s
118300K .......... .......... .......... .......... .......... 44% 7.19M 13s
118350K .......... .......... .......... .......... .......... 44% 14.3M 13s
118400K .......... .......... .......... .......... .......... 44% 7.60M 13s
118450K .......... .......... .......... .......... .......... 44% 13.0M 13s
118500K .......... .......... .......... .......... .......... 44% 8.22M 13s
118550K .......... .......... .......... .......... .......... 44% 12.9M 13s
118600K .......... .......... .......... .......... .......... 44% 8.02M 13s
118650K .......... .......... .......... .......... .......... 44% 11.7M 13s
118700K .......... .......... .......... .......... .......... 44% 10.9M 13s
118750K .......... .......... .......... .......... .......... 44% 9.97M 13s
118800K .......... .......... .......... .......... .......... 44% 11.3M 13s
118850K .......... .......... .......... .......... .......... 44% 9.29M 13s
118900K .......... .......... .......... .......... .......... 44% 8.81M 13s
118950K .......... .......... .......... .......... .......... 44% 9.69M 13s
119000K .......... .......... .......... .......... .......... 44% 15.9M 13s
119050K .......... .......... .......... .......... .......... 44% 7.12M 13s
119100K .......... .......... .......... .......... .......... 44% 13.8M 13s
119150K .......... .......... .......... .......... .......... 44% 9.05M 13s
119200K .......... .......... .......... .......... .......... 44% 11.0M 13s
119250K .......... .......... .......... .......... .......... 44% 8.60M 13s
119300K .......... .......... .......... .......... .......... 44% 10.2M 13s
119350K .......... .......... .......... .......... .......... 44% 13.9M 13s
119400K .......... .......... .......... .......... .......... 44% 9.23M 13s
119450K .......... .......... .......... .......... .......... 44% 10.4M 13s
119500K .......... .......... .......... .......... .......... 44% 7.61M 13s
119550K .......... .......... .......... .......... .......... 45% 13.8M 13s
119600K .......... .......... .......... .......... .......... 45% 6.92M 13s
119650K .......... .......... .......... .......... .......... 45% 16.2M 13s
119700K .......... .......... .......... .......... .......... 45% 6.10M 13s
119750K .......... .......... .......... .......... .......... 45% 17.9M 13s
119800K .......... .......... .......... .......... .......... 45% 14.1M 13s
119850K .......... .......... .......... .......... .......... 45% 8.83M 13s
119900K .......... .......... .......... .......... .......... 45% 12.8M 13s
119950K .......... .......... .......... .......... .......... 45% 7.38M 13s
120000K .......... .......... .......... .......... .......... 45% 16.0M 13s
120050K .......... .......... .......... .......... .......... 45% 6.14M 13s
120100K .......... .......... .......... .......... .......... 45% 18.3M 13s
120150K .......... .......... .......... .......... .......... 45% 12.7M 13s
120200K .......... .......... .......... .......... .......... 45% 7.24M 13s
120250K .......... .......... .......... .......... .......... 45% 19.9M 13s
120300K .......... .......... .......... .......... .......... 45% 6.61M 13s
120350K .......... .......... .......... .......... .......... 45% 15.1M 13s
120400K .......... .......... .......... .......... .......... 45% 11.0M 13s
120450K .......... .......... .......... .......... .......... 45% 7.32M 13s
120500K .......... .......... .......... .......... .......... 45% 15.0M 13s
120550K .......... .......... .......... .......... .......... 45% 6.46M 13s
120600K .......... .......... .......... .......... .......... 45% 14.8M 13s
120650K .......... .......... .......... .......... .......... 45% 7.95M 13s
120700K .......... .......... .......... .......... .......... 45% 13.3M 13s
120750K .......... .......... .......... .......... .......... 45% 8.00M 13s
120800K .......... .......... .......... .......... .......... 45% 10.8M 13s
120850K .......... .......... .......... .......... .......... 45% 12.2M 13s
120900K .......... .......... .......... .......... .......... 45% 7.49M 13s
120950K .......... .......... .......... .......... .......... 45% 10.9M 13s
121000K .......... .......... .......... .......... .......... 45% 11.6M 13s
121050K .......... .......... .......... .......... .......... 45% 8.99M 13s
121100K .......... .......... .......... .......... .......... 45% 7.80M 13s
121150K .......... .......... .......... .......... .......... 45% 11.7M 13s
121200K .......... .......... .......... .......... .......... 45% 8.75M 13s
121250K .......... .......... .......... .......... .......... 45% 12.0M 13s
121300K .......... .......... .......... .......... .......... 45% 9.89M 13s
121350K .......... .......... .......... .......... .......... 45% 13.4M 13s
121400K .......... .......... .......... .......... .......... 45% 8.31M 13s
121450K .......... .......... .......... .......... .......... 45% 10.8M 13s
121500K .......... .......... .......... .......... .......... 45% 9.07M 13s
121550K .......... .......... .......... .......... .......... 45% 10.3M 13s
121600K .......... .......... .......... .......... .......... 45% 8.81M 13s
121650K .......... .......... .......... .......... .......... 45% 11.2M 13s
121700K .......... .......... .......... .......... .......... 45% 10.2M 13s
121750K .......... .......... .......... .......... .......... 45% 11.5M 13s
121800K .......... .......... .......... .......... .......... 45% 8.30M 13s
121850K .......... .......... .......... .......... .......... 45% 10.0M 13s
121900K .......... .......... .......... .......... .......... 45% 11.0M 13s
121950K .......... .......... .......... .......... .......... 45% 10.1M 13s
122000K .......... .......... .......... .......... .......... 45% 11.5M 13s
122050K .......... .......... .......... .......... .......... 45% 10.6M 13s
122100K .......... .......... .......... .......... .......... 45% 8.14M 13s
122150K .......... .......... .......... .......... .......... 45% 10.1M 13s
122200K .......... .......... .......... .......... .......... 46% 12.6M 13s
122250K .......... .......... .......... .......... .......... 46% 8.69M 13s
122300K .......... .......... .......... .......... .......... 46% 10.8M 13s
122350K .......... .......... .......... .......... .......... 46% 10.3M 13s
122400K .......... .......... .......... .......... .......... 46% 8.05M 13s
122450K .......... .......... .......... .......... .......... 46% 12.4M 13s
122500K .......... .......... .......... .......... .......... 46% 9.39M 13s
122550K .......... .......... .......... .......... .......... 46% 9.93M 13s
122600K .......... .......... .......... .......... .......... 46% 12.6M 13s
122650K .......... .......... .......... .......... .......... 46% 8.15M 13s
122700K .......... .......... .......... .......... .......... 46% 9.79M 13s
122750K .......... .......... .......... .......... .......... 46% 9.16M 13s
122800K .......... .......... .......... .......... .......... 46% 12.0M 13s
122850K .......... .......... .......... .......... .......... 46% 9.87M 13s
122900K .......... .......... .......... .......... .......... 46% 10.3M 13s
122950K .......... .......... .......... .......... .......... 46% 9.17M 13s
123000K .......... .......... .......... .......... .......... 46% 12.5M 13s
123050K .......... .......... .......... .......... .......... 46% 7.95M 13s
123100K .......... .......... .......... .......... .......... 46% 11.4M 13s
123150K .......... .......... .......... .......... .......... 46% 11.8M 13s
123200K .......... .......... .......... .......... .......... 46% 7.39M 13s
123250K .......... .......... .......... .......... .......... 46% 12.9M 13s
123300K .......... .......... .......... .......... .......... 46% 13.1M 13s
123350K .......... .......... .......... .......... .......... 46% 7.60M 13s
123400K .......... .......... .......... .......... .......... 46% 11.9M 13s
123450K .......... .......... .......... .......... .......... 46% 8.31M 13s
123500K .......... .......... .......... .......... .......... 46% 11.4M 13s
123550K .......... .......... .......... .......... .......... 46% 15.3M 13s
123600K .......... .......... .......... .......... .......... 46% 7.40M 13s
123650K .......... .......... .......... .......... .......... 46% 9.38M 13s
123700K .......... .......... .......... .......... .......... 46% 8.49M 13s
123750K .......... .......... .......... .......... .......... 46% 14.3M 13s
123800K .......... .......... .......... .......... .......... 46% 9.95M 13s
123850K .......... .......... .......... .......... .......... 46% 9.20M 13s
123900K .......... .......... .......... .......... .......... 46% 11.3M 13s
123950K .......... .......... .......... .......... .......... 46% 12.6M 13s
124000K .......... .......... .......... .......... .......... 46% 7.21M 13s
124050K .......... .......... .......... .......... .......... 46% 18.2M 13s
124100K .......... .......... .......... .......... .......... 46% 8.95M 13s
124150K .......... .......... .......... .......... .......... 46% 8.80M 13s
124200K .......... .......... .......... .......... .......... 46% 9.24M 13s
124250K .......... .......... .......... .......... .......... 46% 11.9M 13s
124300K .......... .......... .......... .......... .......... 46% 10.0M 13s
124350K .......... .......... .......... .......... .......... 46% 8.99M 13s
124400K .......... .......... .......... .......... .......... 46% 10.8M 13s
124450K .......... .......... .......... .......... .......... 46% 11.3M 12s
124500K .......... .......... .......... .......... .......... 46% 9.82M 12s
124550K .......... .......... .......... .......... .......... 46% 9.11M 12s
124600K .......... .......... .......... .......... .......... 46% 11.8M 12s
124650K .......... .......... .......... .......... .......... 46% 10.3M 12s
124700K .......... .......... .......... .......... .......... 46% 8.02M 12s
124750K .......... .......... .......... .......... .......... 46% 12.1M 12s
124800K .......... .......... .......... .......... .......... 46% 13.5M 12s
124850K .......... .......... .......... .......... .......... 47% 6.74M 12s
124900K .......... .......... .......... .......... .......... 47% 15.1M 12s
124950K .......... .......... .......... .......... .......... 47% 10.7M 12s
125000K .......... .......... .......... .......... .......... 47% 5.09M 12s
125050K .......... .......... .......... .......... .......... 47% 12.3M 12s
125100K .......... .......... .......... .......... .......... 47% 7.12M 12s
125150K .......... .......... .......... .......... .......... 47% 5.91M 12s
125200K .......... .......... .......... .......... .......... 47% 12.9M 12s
125250K .......... .......... .......... .......... .......... 47% 10.5M 12s
125300K .......... .......... .......... .......... .......... 47% 7.95M 12s
125350K .......... .......... .......... .......... .......... 47% 9.31M 12s
125400K .......... .......... .......... .......... .......... 47% 10.3M 12s
125450K .......... .......... .......... .......... .......... 47% 5.39M 12s
125500K .......... .......... .......... .......... .......... 47% 16.8M 12s
125550K .......... .......... .......... .......... .......... 47% 13.7M 12s
125600K .......... .......... .......... .......... .......... 47% 6.63M 12s
125650K .......... .......... .......... .......... .......... 47% 9.52M 12s
125700K .......... .......... .......... .......... .......... 47% 10.2M 12s
125750K .......... .......... .......... .......... .......... 47% 7.12M 12s
125800K .......... .......... .......... .......... .......... 47% 14.4M 12s
125850K .......... .......... .......... .......... .......... 47% 11.0M 12s
125900K .......... .......... .......... .......... .......... 47% 7.61M 12s
125950K .......... .......... .......... .......... .......... 47% 9.24M 12s
126000K .......... .......... .......... .......... .......... 47% 11.8M 12s
126050K .......... .......... .......... .......... .......... 47% 7.27M 12s
126100K .......... .......... .......... .......... .......... 47% 16.9M 12s
126150K .......... .......... .......... .......... .......... 47% 7.67M 12s
126200K .......... .......... .......... .......... .......... 47% 7.06M 12s
126250K .......... .......... .......... .......... .......... 47% 9.80M 12s
126300K .......... .......... .......... .......... .......... 47% 11.9M 12s
126350K .......... .......... .......... .......... .......... 47% 8.24M 12s
126400K .......... .......... .......... .......... .......... 47% 11.1M 12s
126450K .......... .......... .......... .......... .......... 47% 11.5M 12s
126500K .......... .......... .......... .......... .......... 47% 8.72M 12s
126550K .......... .......... .......... .......... .......... 47% 9.86M 12s
126600K .......... .......... .......... .......... .......... 47% 12.6M 12s
126650K .......... .......... .......... .......... .......... 47% 8.02M 12s
126700K .......... .......... .......... .......... .......... 47% 10.4M 12s
126750K .......... .......... .......... .......... .......... 47% 12.3M 12s
126800K .......... .......... .......... .......... .......... 47% 8.52M 12s
126850K .......... .......... .......... .......... .......... 47% 9.79M 12s
126900K .......... .......... .......... .......... .......... 47% 17.2M 12s
126950K .......... .......... .......... .......... .......... 47% 7.05M 12s
127000K .......... .......... .......... .......... .......... 47% 11.5M 12s
127050K .......... .......... .......... .......... .......... 47% 13.7M 12s
127100K .......... .......... .......... .......... .......... 47% 6.85M 12s
127150K .......... .......... .......... .......... .......... 47% 11.3M 12s
127200K .......... .......... .......... .......... .......... 47% 11.5M 12s
127250K .......... .......... .......... .......... .......... 47% 9.86M 12s
127300K .......... .......... .......... .......... .......... 47% 8.94M 12s
127350K .......... .......... .......... .......... .......... 47% 12.3M 12s
127400K .......... .......... .......... .......... .......... 47% 8.47M 12s
127450K .......... .......... .......... .......... .......... 47% 9.13M 12s
127500K .......... .......... .......... .......... .......... 47% 13.7M 12s
127550K .......... .......... .......... .......... .......... 48% 8.39M 12s
127600K .......... .......... .......... .......... .......... 48% 9.67M 12s
127650K .......... .......... .......... .......... .......... 48% 11.3M 12s
127700K .......... .......... .......... .......... .......... 48% 7.85M 12s
127750K .......... .......... .......... .......... .......... 48% 23.8M 12s
127800K .......... .......... .......... .......... .......... 48% 11.0M 12s
127850K .......... .......... .......... .......... .......... 48% 5.84M 12s
127900K .......... .......... .......... .......... .......... 48% 21.7M 12s
127950K .......... .......... .......... .......... .......... 48% 11.0M 12s
128000K .......... .......... .......... .......... .......... 48% 8.66M 12s
128050K .......... .......... .......... .......... .......... 48% 11.8M 12s
128100K .......... .......... .......... .......... .......... 48% 10.9M 12s
128150K .......... .......... .......... .......... .......... 48% 7.45M 12s
128200K .......... .......... .......... .......... .......... 48% 11.3M 12s
128250K .......... .......... .......... .......... .......... 48% 12.8M 12s
128300K .......... .......... .......... .......... .......... 48% 8.46M 12s
128350K .......... .......... .......... .......... .......... 48% 8.65M 12s
128400K .......... .......... .......... .......... .......... 48% 18.8M 12s
128450K .......... .......... .......... .......... .......... 48% 7.15M 12s
128500K .......... .......... .......... .......... .......... 48% 10.6M 12s
128550K .......... .......... .......... .......... .......... 48% 13.7M 12s
128600K .......... .......... .......... .......... .......... 48% 8.41M 12s
128650K .......... .......... .......... .......... .......... 48% 8.09M 12s
128700K .......... .......... .......... .......... .......... 48% 13.6M 12s
128750K .......... .......... .......... .......... .......... 48% 19.5M 12s
128800K .......... .......... .......... .......... .......... 48% 5.25M 12s
128850K .......... .......... .......... .......... .......... 48% 17.7M 12s
128900K .......... .......... .......... .......... .......... 48% 15.1M 12s
128950K .......... .......... .......... .......... .......... 48% 6.44M 12s
129000K .......... .......... .......... .......... .......... 48% 11.9M 12s
129050K .......... .......... .......... .......... .......... 48% 15.2M 12s
129100K .......... .......... .......... .......... .......... 48% 7.74M 12s
129150K .......... .......... .......... .......... .......... 48% 9.11M 12s
129200K .......... .......... .......... .......... .......... 48% 16.2M 12s
129250K .......... .......... .......... .......... .......... 48% 8.42M 12s
129300K .......... .......... .......... .......... .......... 48% 7.47M 12s
129350K .......... .......... .......... .......... .......... 48% 16.4M 12s
129400K .......... .......... .......... .......... .......... 48% 14.0M 12s
129450K .......... .......... .......... .......... .......... 48% 5.20M 12s
129500K .......... .......... .......... .......... .......... 48% 20.2M 12s
129550K .......... .......... .......... .......... .......... 48% 12.8M 12s
129600K .......... .......... .......... .......... .......... 48% 6.33M 12s
129650K .......... .......... .......... .......... .......... 48% 12.8M 12s
129700K .......... .......... .......... .......... .......... 48% 21.7M 12s
129750K .......... .......... .......... .......... .......... 48% 8.28M 12s
129800K .......... .......... .......... .......... .......... 48% 6.99M 12s
129850K .......... .......... .......... .......... .......... 48% 18.2M 12s
129900K .......... .......... .......... .......... .......... 48% 11.0M 12s
129950K .......... .......... .......... .......... .......... 48% 5.66M 12s
130000K .......... .......... .......... .......... .......... 48% 22.0M 12s
130050K .......... .......... .......... .......... .......... 48% 11.8M 12s
130100K .......... .......... .......... .......... .......... 48% 7.68M 12s
130150K .......... .......... .......... .......... .......... 48% 9.76M 12s
130200K .......... .......... .......... .......... .......... 49% 11.1M 12s
130250K .......... .......... .......... .......... .......... 49% 28.6M 12s
130300K .......... .......... .......... .......... .......... 49% 5.20M 12s
130350K .......... .......... .......... .......... .......... 49% 18.5M 12s
130400K .......... .......... .......... .......... .......... 49% 11.7M 12s
130450K .......... .......... .......... .......... .......... 49% 7.73M 12s
130500K .......... .......... .......... .......... .......... 49% 10.8M 12s
130550K .......... .......... .......... .......... .......... 49% 12.3M 12s
130600K .......... .......... .......... .......... .......... 49% 14.7M 12s
130650K .......... .......... .......... .......... .......... 49% 5.82M 12s
130700K .......... .......... .......... .......... .......... 49% 18.6M 12s
130750K .......... .......... .......... .......... .......... 49% 12.0M 12s
130800K .......... .......... .......... .......... .......... 49% 5.73M 12s
130850K .......... .......... .......... .......... .......... 49% 16.1M 12s
130900K .......... .......... .......... .......... .......... 49% 13.6M 12s
130950K .......... .......... .......... .......... .......... 49% 8.53M 12s
131000K .......... .......... .......... .......... .......... 49% 8.39M 12s
131050K .......... .......... .......... .......... .......... 49% 21.1M 12s
131100K .......... .......... .......... .......... .......... 49% 10.8M 12s
131150K .......... .......... .......... .......... .......... 49% 5.31M 12s
131200K .......... .......... .......... .......... .......... 49% 22.4M 12s
131250K .......... .......... .......... .......... .......... 49% 12.2M 12s
131300K .......... .......... .......... .......... .......... 49% 9.28M 12s
131350K .......... .......... .......... .......... .......... 49% 7.43M 12s
131400K .......... .......... .......... .......... .......... 49% 12.0M 12s
131450K .......... .......... .......... .......... .......... 49% 15.4M 12s
131500K .......... .......... .......... .......... .......... 49% 6.16M 12s
131550K .......... .......... .......... .......... .......... 49% 18.4M 12s
131600K .......... .......... .......... .......... .......... 49% 10.1M 12s
131650K .......... .......... .......... .......... .......... 49% 8.86M 12s
131700K .......... .......... .......... .......... .......... 49% 9.01M 12s
131750K .......... .......... .......... .......... .......... 49% 10.7M 12s
131800K .......... .......... .......... .......... .......... 49% 10.7M 12s
131850K .......... .......... .......... .......... .......... 49% 7.18M 12s
131900K .......... .......... .......... .......... .......... 49% 23.1M 12s
131950K .......... .......... .......... .......... .......... 49% 9.88M 12s
132000K .......... .......... .......... .......... .......... 49% 8.85M 12s
132050K .......... .......... .......... .......... .......... 49% 9.21M 12s
132100K .......... .......... .......... .......... .......... 49% 10.1M 12s
132150K .......... .......... .......... .......... .......... 49% 11.4M 12s
132200K .......... .......... .......... .......... .......... 49% 8.16M 12s
132250K .......... .......... .......... .......... .......... 49% 18.2M 12s
132300K .......... .......... .......... .......... .......... 49% 8.56M 12s
132350K .......... .......... .......... .......... .......... 49% 9.41M 12s
132400K .......... .......... .......... .......... .......... 49% 9.45M 12s
132450K .......... .......... .......... .......... .......... 49% 11.2M 12s
132500K .......... .......... .......... .......... .......... 49% 9.38M 12s
132550K .......... .......... .......... .......... .......... 49% 2.50M 12s
132600K .......... .......... .......... .......... .......... 49% 108M 12s
132650K .......... .......... .......... .......... .......... 49% 122M 12s
132700K .......... .......... .......... .......... .......... 49% 148M 12s
132750K .......... .......... .......... .......... .......... 49% 10.8M 12s
132800K .......... .......... .......... .......... .......... 49% 8.25M 12s
132850K .......... .......... .......... .......... .......... 50% 6.53M 12s
132900K .......... .......... .......... .......... .......... 50% 11.6M 12s
132950K .......... .......... .......... .......... .......... 50% 9.06M 12s
133000K .......... .......... .......... .......... .......... 50% 7.79M 12s
133050K .......... .......... .......... .......... .......... 50% 9.11M 12s
133100K .......... .......... .......... .......... .......... 50% 6.28M 12s
133150K .......... .......... .......... .......... .......... 50% 11.1M 12s
133200K .......... .......... .......... .......... .......... 50% 7.78M 12s
133250K .......... .......... .......... .......... .......... 50% 9.97M 12s
133300K .......... .......... .......... .......... .......... 50% 8.68M 12s
133350K .......... .......... .......... .......... .......... 50% 7.07M 12s
133400K .......... .......... .......... .......... .......... 50% 7.60M 12s
133450K .......... .......... .......... .......... .......... 50% 11.2M 12s
133500K .......... .......... .......... .......... .......... 50% 8.73M 12s
133550K .......... .......... .......... .......... .......... 50% 8.77M 12s
133600K .......... .......... .......... .......... .......... 50% 8.36M 12s
133650K .......... .......... .......... .......... .......... 50% 6.80M 12s
133700K .......... .......... .......... .......... .......... 50% 9.08M 12s
133750K .......... .......... .......... .......... .......... 50% 8.99M 12s
133800K .......... .......... .......... .......... .......... 50% 9.01M 12s
133850K .......... .......... .......... .......... .......... 50% 7.33M 12s
133900K .......... .......... .......... .......... .......... 50% 10.6M 12s
133950K .......... .......... .......... .......... .......... 50% 7.33M 12s
134000K .......... .......... .......... .......... .......... 50% 7.59M 12s
134050K .......... .......... .......... .......... .......... 50% 8.54M 12s
134100K .......... .......... .......... .......... .......... 50% 9.39M 12s
134150K .......... .......... .......... .......... .......... 50% 8.98M 12s
134200K .......... .......... .......... .......... .......... 50% 8.09M 12s
134250K .......... .......... .......... .......... .......... 50% 7.56M 12s
134300K .......... .......... .......... .......... .......... 50% 7.68M 12s
134350K .......... .......... .......... .......... .......... 50% 10.5M 12s
134400K .......... .......... .......... .......... .......... 50% 8.30M 12s
134450K .......... .......... .......... .......... .......... 50% 7.13M 12s
134500K .......... .......... .......... .......... .......... 50% 10.6M 12s
134550K .......... .......... .......... .......... .......... 50% 7.06M 12s
134600K .......... .......... .......... .......... .......... 50% 8.21M 12s
134650K .......... .......... .......... .......... .......... 50% 9.54M 12s
134700K .......... .......... .......... .......... .......... 50% 6.70M 12s
134750K .......... .......... .......... .......... .......... 50% 10.3M 12s
134800K .......... .......... .......... .......... .......... 50% 12.5M 12s
134850K .......... .......... .......... .......... .......... 50% 5.75M 12s
134900K .......... .......... .......... .......... .......... 50% 9.88M 12s
134950K .......... .......... .......... .......... .......... 50% 7.88M 12s
135000K .......... .......... .......... .......... .......... 50% 8.37M 12s
135050K .......... .......... .......... .......... .......... 50% 13.7M 12s
135100K .......... .......... .......... .......... .......... 50% 8.38M 12s
135150K .......... .......... .......... .......... .......... 50% 6.56M 12s
135200K .......... .......... .......... .......... .......... 50% 8.01M 12s
135250K .......... .......... .......... .......... .......... 50% 18.1M 12s
135300K .......... .......... .......... .......... .......... 50% 5.74M 12s
135350K .......... .......... .......... .......... .......... 50% 9.48M 12s
135400K .......... .......... .......... .......... .......... 50% 12.0M 12s
135450K .......... .......... .......... .......... .......... 50% 6.78M 12s
135500K .......... .......... .......... .......... .......... 51% 10.8M 12s
135550K .......... .......... .......... .......... .......... 51% 8.11M 12s
135600K .......... .......... .......... .......... .......... 51% 8.79M 12s
135650K .......... .......... .......... .......... .......... 51% 9.45M 12s
135700K .......... .......... .......... .......... .......... 51% 6.35M 12s
135750K .......... .......... .......... .......... .......... 51% 8.59M 12s
135800K .......... .......... .......... .......... .......... 51% 15.1M 12s
135850K .......... .......... .......... .......... .......... 51% 6.35M 12s
135900K .......... .......... .......... .......... .......... 51% 9.64M 12s
135950K .......... .......... .......... .......... .......... 51% 10.1M 12s
136000K .......... .......... .......... .......... .......... 51% 6.77M 12s
136050K .......... .......... .......... .......... .......... 51% 9.95M 12s
136100K .......... .......... .......... .......... .......... 51% 8.43M 12s
136150K .......... .......... .......... .......... .......... 51% 9.00M 12s
136200K .......... .......... .......... .......... .......... 51% 7.87M 12s
136250K .......... .......... .......... .......... .......... 51% 8.02M 12s
136300K .......... .......... .......... .......... .......... 51% 11.9M 12s
136350K .......... .......... .......... .......... .......... 51% 1.74M 12s
136400K .......... .......... .......... .......... .......... 51% 111M 12s
136450K .......... .......... .......... .......... .......... 51% 89.6M 12s
136500K .......... .......... .......... .......... .......... 51% 154M 12s
136550K .......... .......... .......... .......... .......... 51% 88.1M 12s
136600K .......... .......... .......... .......... .......... 51% 7.82M 12s
136650K .......... .......... .......... .......... .......... 51% 5.91M 12s
136700K .......... .......... .......... .......... .......... 51% 24.6M 12s
136750K .......... .......... .......... .......... .......... 51% 7.07M 12s
136800K .......... .......... .......... .......... .......... 51% 6.21M 12s
136850K .......... .......... .......... .......... .......... 51% 17.1M 12s
136900K .......... .......... .......... .......... .......... 51% 8.57M 12s
136950K .......... .......... .......... .......... .......... 51% 5.49M 12s
137000K .......... .......... .......... .......... .......... 51% 20.7M 12s
137050K .......... .......... .......... .......... .......... 51% 10.4M 12s
137100K .......... .......... .......... .......... .......... 51% 5.26M 12s
137150K .......... .......... .......... .......... .......... 51% 18.1M 12s
137200K .......... .......... .......... .......... .......... 51% 11.0M 12s
137250K .......... .......... .......... .......... .......... 51% 5.34M 12s
137300K .......... .......... .......... .......... .......... 51% 15.1M 12s
137350K .......... .......... .......... .......... .......... 51% 12.7M 12s
137400K .......... .......... .......... .......... .......... 51% 5.23M 12s
137450K .......... .......... .......... .......... .......... 51% 15.5M 12s
137500K .......... .......... .......... .......... .......... 51% 12.8M 12s
137550K .......... .......... .......... .......... .......... 51% 5.29M 12s
137600K .......... .......... .......... .......... .......... 51% 14.7M 12s
137650K .......... .......... .......... .......... .......... 51% 12.4M 12s
137700K .......... .......... .......... .......... .......... 51% 5.40M 12s
137750K .......... .......... .......... .......... .......... 51% 18.8M 12s
137800K .......... .......... .......... .......... .......... 51% 12.7M 12s
137850K .......... .......... .......... .......... .......... 51% 5.29M 12s
137900K .......... .......... .......... .......... .......... 51% 20.6M 12s
137950K .......... .......... .......... .......... .......... 51% 16.1M 12s
138000K .......... .......... .......... .......... .......... 51% 5.65M 12s
138050K .......... .......... .......... .......... .......... 51% 16.2M 11s
138100K .......... .......... .......... .......... .......... 51% 11.6M 11s
138150K .......... .......... .......... .......... .......... 52% 6.11M 11s
138200K .......... .......... .......... .......... .......... 52% 10.5M 11s
138250K .......... .......... .......... .......... .......... 52% 18.1M 11s
138300K .......... .......... .......... .......... .......... 52% 3.84M 11s
138350K .......... .......... .......... .......... .......... 52% 77.7M 11s
138400K .......... .......... .......... .......... .......... 52% 23.0M 11s
138450K .......... .......... .......... .......... .......... 52% 4.59M 11s
138500K .......... .......... .......... .......... .......... 52% 15.7M 11s
138550K .......... .......... .......... .......... .......... 52% 6.31M 11s
138600K .......... .......... .......... .......... .......... 52% 10.3M 11s
138650K .......... .......... .......... .......... .......... 52% 20.3M 11s
138700K .......... .......... .......... .......... .......... 52% 5.94M 11s
138750K .......... .......... .......... .......... .......... 52% 12.2M 11s
138800K .......... .......... .......... .......... .......... 52% 14.3M 11s
138850K .......... .......... .......... .......... .......... 52% 2.51M 11s
138900K .......... .......... .......... .......... .......... 52% 34.6M 11s
138950K .......... .......... .......... .......... .......... 52% 47.6M 11s
139000K .......... .......... .......... .......... .......... 52% 33.7M 11s
139050K .......... .......... .......... .......... .......... 52% 8.75M 11s
139100K .......... .......... .......... .......... .......... 52% 10.7M 11s
139150K .......... .......... .......... .......... .......... 52% 5.36M 11s
139200K .......... .......... .......... .......... .......... 52% 13.0M 11s
139250K .......... .......... .......... .......... .......... 52% 6.13M 11s
139300K .......... .......... .......... .......... .......... 52% 15.1M 11s
139350K .......... .......... .......... .......... .......... 52% 6.02M 11s
139400K .......... .......... .......... .......... .......... 52% 13.4M 11s
139450K .......... .......... .......... .......... .......... 52% 6.99M 11s
139500K .......... .......... .......... .......... .......... 52% 11.6M 11s
139550K .......... .......... .......... .......... .......... 52% 10.3M 11s
139600K .......... .......... .......... .......... .......... 52% 7.62M 11s
139650K .......... .......... .......... .......... .......... 52% 10.0M 11s
139700K .......... .......... .......... .......... .......... 52% 8.42M 11s
139750K .......... .......... .......... .......... .......... 52% 9.43M 11s
139800K .......... .......... .......... .......... .......... 52% 11.7M 11s
139850K .......... .......... .......... .......... .......... 52% 2.85M 11s
139900K .......... .......... .......... .......... .......... 52% 27.1M 11s
139950K .......... .......... .......... .......... .......... 52% 38.4M 11s
140000K .......... .......... .......... .......... .......... 52% 31.0M 11s
140050K .......... .......... .......... .......... .......... 52% 12.7M 11s
140100K .......... .......... .......... .......... .......... 52% 8.30M 11s
140150K .......... .......... .......... .......... .......... 52% 11.8M 11s
140200K .......... .......... .......... .......... .......... 52% 6.84M 11s
140250K .......... .......... .......... .......... .......... 52% 9.10M 11s
140300K .......... .......... .......... .......... .......... 52% 11.6M 11s
140350K .......... .......... .......... .......... .......... 52% 9.02M 11s
140400K .......... .......... .......... .......... .......... 52% 7.13M 11s
140450K .......... .......... .......... .......... .......... 52% 9.84M 11s
140500K .......... .......... .......... .......... .......... 52% 10.2M 11s
140550K .......... .......... .......... .......... .......... 52% 6.61M 11s
140600K .......... .......... .......... .......... .......... 52% 13.9M 11s
140650K .......... .......... .......... .......... .......... 52% 8.29M 11s
140700K .......... .......... .......... .......... .......... 52% 7.10M 11s
140750K .......... .......... .......... .......... .......... 52% 12.3M 11s
140800K .......... .......... .......... .......... .......... 53% 7.83M 11s
140850K .......... .......... .......... .......... .......... 53% 11.2M 11s
140900K .......... .......... .......... .......... .......... 53% 7.45M 11s
140950K .......... .......... .......... .......... .......... 53% 7.58M 11s
141000K .......... .......... .......... .......... .......... 53% 15.2M 11s
141050K .......... .......... .......... .......... .......... 53% 3.52M 11s
141100K .......... .......... .......... .......... .......... 53% 25.4M 11s
141150K .......... .......... .......... .......... .......... 53% 42.1M 11s
141200K .......... .......... .......... .......... .......... 53% 8.75M 11s
141250K .......... .......... .......... .......... .......... 53% 8.04M 11s
141300K .......... .......... .......... .......... .......... 53% 8.21M 11s
141350K .......... .......... .......... .......... .......... 53% 7.61M 11s
141400K .......... .......... .......... .......... .......... 53% 11.2M 11s
141450K .......... .......... .......... .......... .......... 53% 6.18M 11s
141500K .......... .......... .......... .......... .......... 53% 9.92M 11s
141550K .......... .......... .......... .......... .......... 53% 12.0M 11s
141600K .......... .......... .......... .......... .......... 53% 8.03M 11s
141650K .......... .......... .......... .......... .......... 53% 7.71M 11s
141700K .......... .......... .......... .......... .......... 53% 7.42M 11s
141750K .......... .......... .......... .......... .......... 53% 9.31M 11s
141800K .......... .......... .......... .......... .......... 53% 11.9M 11s
141850K .......... .......... .......... .......... .......... 53% 6.91M 11s
141900K .......... .......... .......... .......... .......... 53% 8.93M 11s
141950K .......... .......... .......... .......... .......... 53% 8.74M 11s
142000K .......... .......... .......... .......... .......... 53% 13.4M 11s
142050K .......... .......... .......... .......... .......... 53% 9.08M 11s
142100K .......... .......... .......... .......... .......... 53% 7.32M 11s
142150K .......... .......... .......... .......... .......... 53% 9.39M 11s
142200K .......... .......... .......... .......... .......... 53% 7.33M 11s
142250K .......... .......... .......... .......... .......... 53% 13.0M 11s
142300K .......... .......... .......... .......... .......... 53% 9.13M 11s
142350K .......... .......... .......... .......... .......... 53% 8.24M 11s
142400K .......... .......... .......... .......... .......... 53% 11.9M 11s
142450K .......... .......... .......... .......... .......... 53% 8.95M 11s
142500K .......... .......... .......... .......... .......... 53% 12.1M 11s
142550K .......... .......... .......... .......... .......... 53% 7.75M 11s
142600K .......... .......... .......... .......... .......... 53% 11.3M 11s
142650K .......... .......... .......... .......... .......... 53% 10.1M 11s
142700K .......... .......... .......... .......... .......... 53% 7.72M 11s
142750K .......... .......... .......... .......... .......... 53% 9.32M 11s
142800K .......... .......... .......... .......... .......... 53% 16.3M 11s
142850K .......... .......... .......... .......... .......... 53% 7.87M 11s
142900K .......... .......... .......... .......... .......... 53% 9.94M 11s
142950K .......... .......... .......... .......... .......... 53% 10.0M 11s
143000K .......... .......... .......... .......... .......... 53% 12.1M 11s
143050K .......... .......... .......... .......... .......... 53% 6.74M 11s
143100K .......... .......... .......... .......... .......... 53% 7.33M 11s
143150K .......... .......... .......... .......... .......... 53% 8.92M 11s
143200K .......... .......... .......... .......... .......... 53% 6.27M 11s
143250K .......... .......... .......... .......... .......... 53% 14.6M 11s
143300K .......... .......... .......... .......... .......... 53% 6.76M 11s
143350K .......... .......... .......... .......... .......... 53% 5.58M 11s
143400K .......... .......... .......... .......... .......... 53% 14.2M 11s
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143500K .......... .......... .......... .......... .......... 54% 5.67M 11s
143550K .......... .......... .......... .......... .......... 54% 13.7M 11s
143600K .......... .......... .......... .......... .......... 54% 6.57M 11s
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143700K .......... .......... .......... .......... .......... 54% 18.3M 11s
143750K .......... .......... .......... .......... .......... 54% 8.36M 11s
143800K .......... .......... .......... .......... .......... 54% 17.2M 11s
143850K .......... .......... .......... .......... .......... 54% 7.52M 11s
143900K .......... .......... .......... .......... .......... 54% 7.07M 11s
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144000K .......... .......... .......... .......... .......... 54% 8.13M 11s
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144100K .......... .......... .......... .......... .......... 54% 7.84M 11s
144150K .......... .......... .......... .......... .......... 54% 8.50M 11s
144200K .......... .......... .......... .......... .......... 54% 13.9M 11s
144250K .......... .......... .......... .......... .......... 54% 6.93M 11s
144300K .......... .......... .......... .......... .......... 54% 17.8M 11s
144350K .......... .......... .......... .......... .......... 54% 9.22M 11s
144400K .......... .......... .......... .......... .......... 54% 11.6M 11s
144450K .......... .......... .......... .......... .......... 54% 7.74M 11s
144500K .......... .......... .......... .......... .......... 54% 8.36M 11s
144550K .......... .......... .......... .......... .......... 54% 19.3M 11s
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144800K .......... .......... .......... .......... .......... 54% 8.79M 11s
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144900K .......... .......... .......... .......... .......... 54% 20.2M 11s
144950K .......... .......... .......... .......... .......... 54% 7.53M 11s
145000K .......... .......... .......... .......... .......... 54% 20.8M 11s
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145100K .......... .......... .......... .......... .......... 54% 22.9M 11s
145150K .......... .......... .......... .......... .......... 54% 6.15M 11s
145200K .......... .......... .......... .......... .......... 54% 18.1M 11s
145250K .......... .......... .......... .......... .......... 54% 7.50M 11s
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145350K .......... .......... .......... .......... .......... 54% 6.53M 11s
145400K .......... .......... .......... .......... .......... 54% 8.45M 11s
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145550K .......... .......... .......... .......... .......... 54% 17.5M 11s
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145650K .......... .......... .......... .......... .......... 54% 13.5M 11s
145700K .......... .......... .......... .......... .......... 54% 6.97M 11s
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145800K .......... .......... .......... .......... .......... 54% 9.84M 11s
145850K .......... .......... .......... .......... .......... 54% 11.0M 11s
145900K .......... .......... .......... .......... .......... 54% 10.6M 11s
145950K .......... .......... .......... .......... .......... 54% 9.66M 11s
146000K .......... .......... .......... .......... .......... 54% 11.0M 11s
146050K .......... .......... .......... .......... .......... 54% 9.87M 11s
146100K .......... .......... .......... .......... .......... 54% 8.77M 11s
146150K .......... .......... .......... .......... .......... 55% 12.0M 11s
146200K .......... .......... .......... .......... .......... 55% 9.02M 11s
146250K .......... .......... .......... .......... .......... 55% 13.0M 11s
146300K .......... .......... .......... .......... .......... 55% 9.19M 11s
146350K .......... .......... .......... .......... .......... 55% 11.5M 11s
146400K .......... .......... .......... .......... .......... 55% 8.97M 11s
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146500K .......... .......... .......... .......... .......... 55% 9.05M 11s
146550K .......... .......... .......... .......... .......... 55% 12.0M 11s
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146650K .......... .......... .......... .......... .......... 55% 11.4M 11s
146700K .......... .......... .......... .......... .......... 55% 8.85M 11s
146750K .......... .......... .......... .......... .......... 55% 12.5M 11s
146800K .......... .......... .......... .......... .......... 55% 9.60M 11s
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146900K .......... .......... .......... .......... .......... 55% 12.1M 11s
146950K .......... .......... .......... .......... .......... 55% 8.11M 11s
147000K .......... .......... .......... .......... .......... 55% 13.8M 11s
147050K .......... .......... .......... .......... .......... 55% 8.75M 11s
147100K .......... .......... .......... .......... .......... 55% 12.0M 11s
147150K .......... .......... .......... .......... .......... 55% 8.95M 11s
147200K .......... .......... .......... .......... .......... 55% 10.5M 11s
147250K .......... .......... .......... .......... .......... 55% 9.25M 11s
147300K .......... .......... .......... .......... .......... 55% 15.8M 11s
147350K .......... .......... .......... .......... .......... 55% 6.91M 11s
147400K .......... .......... .......... .......... .......... 55% 15.9M 11s
147450K .......... .......... .......... .......... .......... 55% 6.81M 11s
147500K .......... .......... .......... .......... .......... 55% 14.7M 11s
147550K .......... .......... .......... .......... .......... 55% 11.4M 11s
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147650K .......... .......... .......... .......... .......... 55% 14.5M 11s
147700K .......... .......... .......... .......... .......... 55% 9.11M 11s
147750K .......... .......... .......... .......... .......... 55% 19.8M 11s
147800K .......... .......... .......... .......... .......... 55% 6.35M 11s
147850K .......... .......... .......... .......... .......... 55% 15.9M 11s
147900K .......... .......... .......... .......... .......... 55% 6.59M 11s
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148000K .......... .......... .......... .......... .......... 55% 7.33M 11s
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148100K .......... .......... .......... .......... .......... 55% 9.59M 11s
148150K .......... .......... .......... .......... .......... 55% 9.48M 11s
148200K .......... .......... .......... .......... .......... 55% 13.7M 11s
148250K .......... .......... .......... .......... .......... 55% 7.37M 11s
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148400K .......... .......... .......... .......... .......... 55% 18.9M 11s
148450K .......... .......... .......... .......... .......... 55% 7.11M 11s
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148850K .......... .......... .......... .......... .......... 56% 8.84M 11s
148900K .......... .......... .......... .......... .......... 56% 19.7M 11s
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149000K .......... .......... .......... .......... .......... 56% 19.4M 11s
149050K .......... .......... .......... .......... .......... 56% 7.92M 11s
149100K .......... .......... .......... .......... .......... 56% 17.5M 11s
149150K .......... .......... .......... .......... .......... 56% 8.26M 11s
149200K .......... .......... .......... .......... .......... 56% 18.5M 11s
149250K .......... .......... .......... .......... .......... 56% 14.0M 11s
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149500K .......... .......... .......... .......... .......... 56% 9.08M 11s
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149900K .......... .......... .......... .......... .......... 56% 12.7M 11s
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150000K .......... .......... .......... .......... .......... 56% 11.9M 11s
150050K .......... .......... .......... .......... .......... 56% 16.4M 11s
150100K .......... .......... .......... .......... .......... 56% 9.01M 11s
150150K .......... .......... .......... .......... .......... 56% 16.5M 11s
150200K .......... .......... .......... .......... .......... 56% 18.2M 11s
150250K .......... .......... .......... .......... .......... 56% 11.2M 10s
150300K .......... .......... .......... .......... .......... 56% 14.9M 10s
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150400K .......... .......... .......... .......... .......... 56% 18.8M 10s
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150500K .......... .......... .......... .......... .......... 56% 11.0M 10s
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150950K .......... .......... .......... .......... .......... 56% 24.1M 10s
151000K .......... .......... .......... .......... .......... 56% 8.67M 10s
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151100K .......... .......... .......... .......... .......... 56% 21.4M 10s
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151200K .......... .......... .......... .......... .......... 56% 15.5M 10s
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151300K .......... .......... .......... .......... .......... 56% 11.5M 10s
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151400K .......... .......... .......... .......... .......... 56% 11.3M 10s
151450K .......... .......... .......... .......... .......... 57% 10.8M 10s
151500K .......... .......... .......... .......... .......... 57% 14.0M 10s
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151600K .......... .......... .......... .......... .......... 57% 17.3M 10s
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151700K .......... .......... .......... .......... .......... 57% 12.1M 10s
151750K .......... .......... .......... .......... .......... 57% 20.9M 10s
151800K .......... .......... .......... .......... .......... 57% 13.2M 10s
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151900K .......... .......... .......... .......... .......... 57% 23.2M 10s
151950K .......... .......... .......... .......... .......... 57% 9.50M 10s
152000K .......... .......... .......... .......... .......... 57% 28.0M 10s
152050K .......... .......... .......... .......... .......... 57% 13.2M 10s
152100K .......... .......... .......... .......... .......... 57% 11.7M 10s
152150K .......... .......... .......... .......... .......... 57% 18.4M 10s
152200K .......... .......... .......... .......... .......... 57% 9.84M 10s
152250K .......... .......... .......... .......... .......... 57% 17.1M 10s
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152350K .......... .......... .......... .......... .......... 57% 11.9M 10s
152400K .......... .......... .......... .......... .......... 57% 27.8M 10s
152450K .......... .......... .......... .......... .......... 57% 11.3M 10s
152500K .......... .......... .......... .......... .......... 57% 14.4M 10s
152550K .......... .......... .......... .......... .......... 57% 22.7M 10s
152600K .......... .......... .......... .......... .......... 57% 10.8M 10s
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152700K .......... .......... .......... .......... .......... 57% 10.8M 10s
152750K .......... .......... .......... .......... .......... 57% 14.0M 10s
152800K .......... .......... .......... .......... .......... 57% 15.3M 10s
152850K .......... .......... .......... .......... .......... 57% 10.4M 10s
152900K .......... .......... .......... .......... .......... 57% 18.5M 10s
152950K .......... .......... .......... .......... .......... 57% 20.9M 10s
153000K .......... .......... .......... .......... .......... 57% 9.79M 10s
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153100K .......... .......... .......... .......... .......... 57% 20.9M 10s
153150K .......... .......... .......... .......... .......... 57% 11.2M 10s
153200K .......... .......... .......... .......... .......... 57% 18.4M 10s
153250K .......... .......... .......... .......... .......... 57% 17.2M 10s
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153350K .......... .......... .......... .......... .......... 57% 3.66M 10s
153400K .......... .......... .......... .......... .......... 57% 54.8M 10s
153450K .......... .......... .......... .......... .......... 57% 40.7M 10s
153500K .......... .......... .......... .......... .......... 57% 49.2M 10s
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153600K .......... .......... .......... .......... .......... 57% 11.8M 10s
153650K .......... .......... .......... .......... .......... 57% 7.36M 10s
153700K .......... .......... .......... .......... .......... 57% 17.0M 10s
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153850K .......... .......... .......... .......... .......... 57% 6.21M 10s
153900K .......... .......... .......... .......... .......... 57% 54.6M 10s
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154000K .......... .......... .......... .......... .......... 57% 31.6M 10s
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154100K .......... .......... .......... .......... .......... 58% 12.8M 10s
154150K .......... .......... .......... .......... .......... 58% 9.83M 10s
154200K .......... .......... .......... .......... .......... 58% 11.7M 10s
154250K .......... .......... .......... .......... .......... 58% 9.58M 10s
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154350K .......... .......... .......... .......... .......... 58% 8.66M 10s
154400K .......... .......... .......... .......... .......... 58% 11.2M 10s
154450K .......... .......... .......... .......... .......... 58% 8.38M 10s
154500K .......... .......... .......... .......... .......... 58% 10.4M 10s
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154600K .......... .......... .......... .......... .......... 58% 12.2M 10s
154650K .......... .......... .......... .......... .......... 58% 9.91M 10s
154700K .......... .......... .......... .......... .......... 58% 10.5M 10s
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154800K .......... .......... .......... .......... .......... 58% 11.5M 10s
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154900K .......... .......... .......... .......... .......... 58% 10.3M 10s
154950K .......... .......... .......... .......... .......... 58% 9.75M 10s
155000K .......... .......... .......... .......... .......... 58% 11.2M 10s
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155100K .......... .......... .......... .......... .......... 58% 11.0M 10s
155150K .......... .......... .......... .......... .......... 58% 9.29M 10s
155200K .......... .......... .......... .......... .......... 58% 11.5M 10s
155250K .......... .......... .......... .......... .......... 58% 8.98M 10s
155300K .......... .......... .......... .......... .......... 58% 12.5M 10s
155350K .......... .......... .......... .......... .......... 58% 8.12M 10s
155400K .......... .......... .......... .......... .......... 58% 12.6M 10s
155450K .......... .......... .......... .......... .......... 58% 8.32M 10s
155500K .......... .......... .......... .......... .......... 58% 14.0M 10s
155550K .......... .......... .......... .......... .......... 58% 9.80M 10s
155600K .......... .......... .......... .......... .......... 58% 9.75M 10s
155650K .......... .......... .......... .......... .......... 58% 9.06M 10s
155700K .......... .......... .......... .......... .......... 58% 10.7M 10s
155750K .......... .......... .......... .......... .......... 58% 9.75M 10s
155800K .......... .......... .......... .......... .......... 58% 16.0M 10s
155850K .......... .......... .......... .......... .......... 58% 11.4M 10s
155900K .......... .......... .......... .......... .......... 58% 12.4M 10s
155950K .......... .......... .......... .......... .......... 58% 10.1M 10s
156000K .......... .......... .......... .......... .......... 58% 9.42M 10s
156050K .......... .......... .......... .......... .......... 58% 10.9M 10s
156100K .......... .......... .......... .......... .......... 58% 8.99M 10s
156150K .......... .......... .......... .......... .......... 58% 11.2M 10s
156200K .......... .......... .......... .......... .......... 58% 8.40M 10s
156250K .......... .......... .......... .......... .......... 58% 18.7M 10s
156300K .......... .......... .......... .......... .......... 58% 14.7M 10s
156350K .......... .......... .......... .......... .......... 58% 7.50M 10s
156400K .......... .......... .......... .......... .......... 58% 12.8M 10s
156450K .......... .......... .......... .......... .......... 58% 8.15M 10s
156500K .......... .......... .......... .......... .......... 58% 11.5M 10s
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156600K .......... .......... .......... .......... .......... 58% 14.1M 10s
156650K .......... .......... .......... .......... .......... 58% 9.55M 10s
156700K .......... .......... .......... .......... .......... 58% 10.1M 10s
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156800K .......... .......... .......... .......... .......... 59% 8.52M 10s
156850K .......... .......... .......... .......... .......... 59% 10.1M 10s
156900K .......... .......... .......... .......... .......... 59% 9.44M 10s
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157000K .......... .......... .......... .......... .......... 59% 11.5M 10s
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157100K .......... .......... .......... .......... .......... 59% 9.17M 10s
157150K .......... .......... .......... .......... .......... 59% 11.2M 10s
157200K .......... .......... .......... .......... .......... 59% 9.18M 10s
157250K .......... .......... .......... .......... .......... 59% 9.96M 10s
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157750K .......... .......... .......... .......... .......... 59% 14.7M 10s
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158000K .......... .......... .......... .......... .......... 59% 12.1M 10s
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158100K .......... .......... .......... .......... .......... 59% 9.15M 10s
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158250K .......... .......... .......... .......... .......... 59% 14.3M 10s
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170450K .......... .......... .......... .......... .......... 64% 10.9M 9s
170500K .......... .......... .......... .......... .......... 64% 15.8M 9s
170550K .......... .......... .......... .......... .......... 64% 14.5M 9s
170600K .......... .......... .......... .......... .......... 64% 11.5M 9s
170650K .......... .......... .......... .......... .......... 64% 15.4M 9s
170700K .......... .......... .......... .......... .......... 64% 9.64M 9s
170750K .......... .......... .......... .......... .......... 64% 24.2M 9s
170800K .......... .......... .......... .......... .......... 64% 9.65M 9s
170850K .......... .......... .......... .......... .......... 64% 11.0M 9s
170900K .......... .......... .......... .......... .......... 64% 28.5M 9s
170950K .......... .......... .......... .......... .......... 64% 7.57M 9s
171000K .......... .......... .......... .......... .......... 64% 26.5M 9s
171050K .......... .......... .......... .......... .......... 64% 3.66M 9s
171100K .......... .......... .......... .......... .......... 64% 38.3M 9s
171150K .......... .......... .......... .......... .......... 64% 85.3M 9s
171200K .......... .......... .......... .......... .......... 64% 29.2M 9s
171250K .......... .......... .......... .......... .......... 64% 9.63M 9s
171300K .......... .......... .......... .......... .......... 64% 14.9M 9s
171350K .......... .......... .......... .......... .......... 64% 9.50M 9s
171400K .......... .......... .......... .......... .......... 64% 16.7M 9s
171450K .......... .......... .......... .......... .......... 64% 8.89M 9s
171500K .......... .......... .......... .......... .......... 64% 14.4M 9s
171550K .......... .......... .......... .......... .......... 64% 8.10M 9s
171600K .......... .......... .......... .......... .......... 64% 12.8M 9s
171650K .......... .......... .......... .......... .......... 64% 11.2M 9s
171700K .......... .......... .......... .......... .......... 64% 13.2M 9s
171750K .......... .......... .......... .......... .......... 64% 10.9M 8s
171800K .......... .......... .......... .......... .......... 64% 10.5M 8s
171850K .......... .......... .......... .......... .......... 64% 8.75M 8s
171900K .......... .......... .......... .......... .......... 64% 12.7M 8s
171950K .......... .......... .......... .......... .......... 64% 14.1M 8s
172000K .......... .......... .......... .......... .......... 64% 13.6M 8s
172050K .......... .......... .......... .......... .......... 64% 10.8M 8s
172100K .......... .......... .......... .......... .......... 64% 21.8M 8s
172150K .......... .......... .......... .......... .......... 64% 15.0M 8s
172200K .......... .......... .......... .......... .......... 64% 10.4M 8s
172250K .......... .......... .......... .......... .......... 64% 33.6M 8s
172300K .......... .......... .......... .......... .......... 64% 10.6M 8s
172350K .......... .......... .......... .......... .......... 64% 15.6M 8s
172400K .......... .......... .......... .......... .......... 64% 13.4M 8s
172450K .......... .......... .......... .......... .......... 64% 19.7M 8s
172500K .......... .......... .......... .......... .......... 64% 11.9M 8s
172550K .......... .......... .......... .......... .......... 64% 24.1M 8s
172600K .......... .......... .......... .......... .......... 64% 10.6M 8s
172650K .......... .......... .......... .......... .......... 64% 45.9M 8s
172700K .......... .......... .......... .......... .......... 65% 8.31M 8s
172750K .......... .......... .......... .......... .......... 65% 13.5M 8s
172800K .......... .......... .......... .......... .......... 65% 24.3M 8s
172850K .......... .......... .......... .......... .......... 65% 11.3M 8s
172900K .......... .......... .......... .......... .......... 65% 16.3M 8s
172950K .......... .......... .......... .......... .......... 65% 14.1M 8s
173000K .......... .......... .......... .......... .......... 65% 5.20M 8s
173050K .......... .......... .......... .......... .......... 65% 21.1M 8s
173100K .......... .......... .......... .......... .......... 65% 25.9M 8s
173150K .......... .......... .......... .......... .......... 65% 45.4M 8s
173200K .......... .......... .......... .......... .......... 65% 29.1M 8s
173250K .......... .......... .......... .......... .......... 65% 11.2M 8s
173300K .......... .......... .......... .......... .......... 65% 21.8M 8s
173350K .......... .......... .......... .......... .......... 65% 13.7M 8s
173400K .......... .......... .......... .......... .......... 65% 16.1M 8s
173450K .......... .......... .......... .......... .......... 65% 11.7M 8s
173500K .......... .......... .......... .......... .......... 65% 11.4M 8s
173550K .......... .......... .......... .......... .......... 65% 20.8M 8s
173600K .......... .......... .......... .......... .......... 65% 15.4M 8s
173650K .......... .......... .......... .......... .......... 65% 15.2M 8s
173700K .......... .......... .......... .......... .......... 65% 10.0M 8s
173750K .......... .......... .......... .......... .......... 65% 14.3M 8s
173800K .......... .......... .......... .......... .......... 65% 20.2M 8s
173850K .......... .......... .......... .......... .......... 65% 11.6M 8s
173900K .......... .......... .......... .......... .......... 65% 13.0M 8s
173950K .......... .......... .......... .......... .......... 65% 11.3M 8s
174000K .......... .......... .......... .......... .......... 65% 41.3M 8s
174050K .......... .......... .......... .......... .......... 65% 11.0M 8s
174100K .......... .......... .......... .......... .......... 65% 13.2M 8s
174150K .......... .......... .......... .......... .......... 65% 31.7M 8s
174200K .......... .......... .......... .......... .......... 65% 11.5M 8s
174250K .......... .......... .......... .......... .......... 65% 10.8M 8s
174300K .......... .......... .......... .......... .......... 65% 21.8M 8s
174350K .......... .......... .......... .......... .......... 65% 15.3M 8s
174400K .......... .......... .......... .......... .......... 65% 11.1M 8s
174450K .......... .......... .......... .......... .......... 65% 15.7M 8s
174500K .......... .......... .......... .......... .......... 65% 11.8M 8s
174550K .......... .......... .......... .......... .......... 65% 20.8M 8s
174600K .......... .......... .......... .......... .......... 65% 17.5M 8s
174650K .......... .......... .......... .......... .......... 65% 11.3M 8s
174700K .......... .......... .......... .......... .......... 65% 19.6M 8s
174750K .......... .......... .......... .......... .......... 65% 16.2M 8s
174800K .......... .......... .......... .......... .......... 65% 10.8M 8s
174850K .......... .......... .......... .......... .......... 65% 26.6M 8s
174900K .......... .......... .......... .......... .......... 65% 14.8M 8s
174950K .......... .......... .......... .......... .......... 65% 12.9M 8s
175000K .......... .......... .......... .......... .......... 65% 34.1M 8s
175050K .......... .......... .......... .......... .......... 65% 13.4M 8s
175100K .......... .......... .......... .......... .......... 65% 19.5M 8s
175150K .......... .......... .......... .......... .......... 65% 14.6M 8s
175200K .......... .......... .......... .......... .......... 65% 26.2M 8s
175250K .......... .......... .......... .......... .......... 65% 14.1M 8s
175300K .......... .......... .......... .......... .......... 65% 20.0M 8s
175350K .......... .......... .......... .......... .......... 66% 17.1M 8s
175400K .......... .......... .......... .......... .......... 66% 20.0M 8s
175450K .......... .......... .......... .......... .......... 66% 14.2M 8s
175500K .......... .......... .......... .......... .......... 66% 37.9M 8s
175550K .......... .......... .......... .......... .......... 66% 11.6M 8s
175600K .......... .......... .......... .......... .......... 66% 9.63M 8s
175650K .......... .......... .......... .......... .......... 66% 83.3M 8s
175700K .......... .......... .......... .......... .......... 66% 12.7M 8s
175750K .......... .......... .......... .......... .......... 66% 69.6M 8s
175800K .......... .......... .......... .......... .......... 66% 10.2M 8s
175850K .......... .......... .......... .......... .......... 66% 14.1M 8s
175900K .......... .......... .......... .......... .......... 66% 34.3M 8s
175950K .......... .......... .......... .......... .......... 66% 10.7M 8s
176000K .......... .......... .......... .......... .......... 66% 60.8M 8s
176050K .......... .......... .......... .......... .......... 66% 11.6M 8s
176100K .......... .......... .......... .......... .......... 66% 20.3M 8s
176150K .......... .......... .......... .......... .......... 66% 16.9M 8s
176200K .......... .......... .......... .......... .......... 66% 13.0M 8s
176250K .......... .......... .......... .......... .......... 66% 30.1M 8s
176300K .......... .......... .......... .......... .......... 66% 14.0M 8s
176350K .......... .......... .......... .......... .......... 66% 15.0M 8s
176400K .......... .......... .......... .......... .......... 66% 17.3M 8s
176450K .......... .......... .......... .......... .......... 66% 19.0M 8s
176500K .......... .......... .......... .......... .......... 66% 16.1M 8s
176550K .......... .......... .......... .......... .......... 66% 21.3M 8s
176600K .......... .......... .......... .......... .......... 66% 13.9M 8s
176650K .......... .......... .......... .......... .......... 66% 24.9M 8s
176700K .......... .......... .......... .......... .......... 66% 12.3M 8s
176750K .......... .......... .......... .......... .......... 66% 14.0M 8s
176800K .......... .......... .......... .......... .......... 66% 42.2M 8s
176850K .......... .......... .......... .......... .......... 66% 15.9M 8s
176900K .......... .......... .......... .......... .......... 66% 15.4M 8s
176950K .......... .......... .......... .......... .......... 66% 16.5M 8s
177000K .......... .......... .......... .......... .......... 66% 19.3M 8s
177050K .......... .......... .......... .......... .......... 66% 13.0M 8s
177100K .......... .......... .......... .......... .......... 66% 18.3M 8s
177150K .......... .......... .......... .......... .......... 66% 18.3M 8s
177200K .......... .......... .......... .......... .......... 66% 12.0M 8s
177250K .......... .......... .......... .......... .......... 66% 16.7M 8s
177300K .......... .......... .......... .......... .......... 66% 23.7M 8s
177350K .......... .......... .......... .......... .......... 66% 14.7M 8s
177400K .......... .......... .......... .......... .......... 66% 14.9M 8s
177450K .......... .......... .......... .......... .......... 66% 13.9M 8s
177500K .......... .......... .......... .......... .......... 66% 27.4M 8s
177550K .......... .......... .......... .......... .......... 66% 13.4M 8s
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177650K .......... .......... .......... .......... .......... 66% 19.7M 8s
177700K .......... .......... .......... .......... .......... 66% 16.7M 8s
177750K .......... .......... .......... .......... .......... 66% 24.5M 8s
177800K .......... .......... .......... .......... .......... 66% 13.4M 8s
177850K .......... .......... .......... .......... .......... 66% 17.7M 8s
177900K .......... .......... .......... .......... .......... 66% 16.9M 8s
177950K .......... .......... .......... .......... .......... 66% 22.1M 8s
178000K .......... .......... .......... .......... .......... 67% 18.3M 8s
178050K .......... .......... .......... .......... .......... 67% 14.6M 8s
178100K .......... .......... .......... .......... .......... 67% 33.6M 8s
178150K .......... .......... .......... .......... .......... 67% 11.1M 8s
178200K .......... .......... .......... .......... .......... 67% 25.5M 8s
178250K .......... .......... .......... .......... .......... 67% 12.0M 8s
178300K .......... .......... .......... .......... .......... 67% 24.4M 8s
178350K .......... .......... .......... .......... .......... 67% 12.7M 8s
178400K .......... .......... .......... .......... .......... 67% 23.5M 8s
178450K .......... .......... .......... .......... .......... 67% 9.42M 8s
178500K .......... .......... .......... .......... .......... 67% 47.2M 8s
178550K .......... .......... .......... .......... .......... 67% 13.6M 8s
178600K .......... .......... .......... .......... .......... 67% 42.3M 8s
178650K .......... .......... .......... .......... .......... 67% 12.4M 8s
178700K .......... .......... .......... .......... .......... 67% 33.9M 8s
178750K .......... .......... .......... .......... .......... 67% 28.5M 8s
178800K .......... .......... .......... .......... .......... 67% 18.5M 8s
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178900K .......... .......... .......... .......... .......... 67% 19.7M 8s
178950K .......... .......... .......... .......... .......... 67% 17.7M 8s
179000K .......... .......... .......... .......... .......... 67% 21.6M 8s
179050K .......... .......... .......... .......... .......... 67% 37.8M 8s
179100K .......... .......... .......... .......... .......... 67% 23.2M 8s
179150K .......... .......... .......... .......... .......... 67% 18.1M 8s
179200K .......... .......... .......... .......... .......... 67% 22.3M 8s
179250K .......... .......... .......... .......... .......... 67% 18.0M 8s
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179350K .......... .......... .......... .......... .......... 67% 13.6M 8s
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179450K .......... .......... .......... .......... .......... 67% 13.3M 8s
179500K .......... .......... .......... .......... .......... 67% 16.1M 8s
179550K .......... .......... .......... .......... .......... 67% 57.9M 8s
179600K .......... .......... .......... .......... .......... 67% 22.5M 8s
179650K .......... .......... .......... .......... .......... 67% 14.1M 8s
179700K .......... .......... .......... .......... .......... 67% 26.0M 8s
179750K .......... .......... .......... .......... .......... 67% 21.7M 8s
179800K .......... .......... .......... .......... .......... 67% 16.6M 8s
179850K .......... .......... .......... .......... .......... 67% 19.5M 8s
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179950K .......... .......... .......... .......... .......... 67% 16.8M 8s
180000K .......... .......... .......... .......... .......... 67% 18.2M 8s
180050K .......... .......... .......... .......... .......... 67% 25.5M 8s
180100K .......... .......... .......... .......... .......... 67% 14.6M 8s
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180200K .......... .......... .......... .......... .......... 67% 12.2M 8s
180250K .......... .......... .......... .......... .......... 67% 26.4M 8s
180300K .......... .......... .......... .......... .......... 67% 15.5M 8s
180350K .......... .......... .......... .......... .......... 67% 23.8M 8s
180400K .......... .......... .......... .......... .......... 67% 40.8M 8s
180450K .......... .......... .......... .......... .......... 67% 13.6M 8s
180500K .......... .......... .......... .......... .......... 67% 31.1M 8s
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180600K .......... .......... .......... .......... .......... 67% 15.0M 8s
180650K .......... .......... .......... .......... .......... 67% 26.5M 8s
180700K .......... .......... .......... .......... .......... 68% 39.4M 8s
180750K .......... .......... .......... .......... .......... 68% 25.3M 8s
180800K .......... .......... .......... .......... .......... 68% 16.4M 8s
180850K .......... .......... .......... .......... .......... 68% 17.6M 8s
180900K .......... .......... .......... .......... .......... 68% 19.7M 8s
180950K .......... .......... .......... .......... .......... 68% 6.47M 8s
181000K .......... .......... .......... .......... .......... 68% 19.5M 8s
181050K .......... .......... .......... .......... .......... 68% 93.8M 8s
181100K .......... .......... .......... .......... .......... 68% 132M 8s
181150K .......... .......... .......... .......... .......... 68% 104M 8s
181200K .......... .......... .......... .......... .......... 68% 12.1M 8s
181250K .......... .......... .......... .......... .......... 68% 42.8M 7s
181300K .......... .......... .......... .......... .......... 68% 16.2M 7s
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181400K .......... .......... .......... .......... .......... 68% 13.3M 7s
181450K .......... .......... .......... .......... .......... 68% 59.3M 7s
181500K .......... .......... .......... .......... .......... 68% 12.9M 7s
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181600K .......... .......... .......... .......... .......... 68% 21.8M 7s
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181700K .......... .......... .......... .......... .......... 68% 37.7M 7s
181750K .......... .......... .......... .......... .......... 68% 16.3M 7s
181800K .......... .......... .......... .......... .......... 68% 70.0M 7s
181850K .......... .......... .......... .......... .......... 68% 12.5M 7s
181900K .......... .......... .......... .......... .......... 68% 38.7M 7s
181950K .......... .......... .......... .......... .......... 68% 15.9M 7s
182000K .......... .......... .......... .......... .......... 68% 18.6M 7s
182050K .......... .......... .......... .......... .......... 68% 30.1M 7s
182100K .......... .......... .......... .......... .......... 68% 13.0M 7s
182150K .......... .......... .......... .......... .......... 68% 28.2M 7s
182200K .......... .......... .......... .......... .......... 68% 17.0M 7s
182250K .......... .......... .......... .......... .......... 68% 14.2M 7s
182300K .......... .......... .......... .......... .......... 68% 36.8M 7s
182350K .......... .......... .......... .......... .......... 68% 15.1M 7s
182400K .......... .......... .......... .......... .......... 68% 23.8M 7s
182450K .......... .......... .......... .......... .......... 68% 13.2M 7s
182500K .......... .......... .......... .......... .......... 68% 32.6M 7s
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182600K .......... .......... .......... .......... .......... 68% 24.1M 7s
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182700K .......... .......... .......... .......... .......... 68% 10.3M 7s
182750K .......... .......... .......... .......... .......... 68% 29.8M 7s
182800K .......... .......... .......... .......... .......... 68% 16.8M 7s
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182900K .......... .......... .......... .......... .......... 68% 19.3M 7s
182950K .......... .......... .......... .......... .......... 68% 11.1M 7s
183000K .......... .......... .......... .......... .......... 68% 32.1M 7s
183050K .......... .......... .......... .......... .......... 68% 17.3M 7s
183100K .......... .......... .......... .......... .......... 68% 19.7M 7s
183150K .......... .......... .......... .......... .......... 68% 17.0M 7s
183200K .......... .......... .......... .......... .......... 68% 12.9M 7s
183250K .......... .......... .......... .......... .......... 68% 33.0M 7s
183300K .......... .......... .......... .......... .......... 68% 22.7M 7s
183350K .......... .......... .......... .......... .......... 69% 16.2M 7s
183400K .......... .......... .......... .......... .......... 69% 15.5M 7s
183450K .......... .......... .......... .......... .......... 69% 31.0M 7s
183500K .......... .......... .......... .......... .......... 69% 16.3M 7s
183550K .......... .......... .......... .......... .......... 69% 25.3M 7s
183600K .......... .......... .......... .......... .......... 69% 14.2M 7s
183650K .......... .......... .......... .......... .......... 69% 32.9M 7s
183700K .......... .......... .......... .......... .......... 69% 13.5M 7s
183750K .......... .......... .......... .......... .......... 69% 21.3M 7s
183800K .......... .......... .......... .......... .......... 69% 20.4M 7s
183850K .......... .......... .......... .......... .......... 69% 17.5M 7s
183900K .......... .......... .......... .......... .......... 69% 21.7M 7s
183950K .......... .......... .......... .......... .......... 69% 17.6M 7s
184000K .......... .......... .......... .......... .......... 69% 21.1M 7s
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184100K .......... .......... .......... .......... .......... 69% 15.3M 7s
184150K .......... .......... .......... .......... .......... 69% 19.9M 7s
184200K .......... .......... .......... .......... .......... 69% 16.1M 7s
184250K .......... .......... .......... .......... .......... 69% 17.4M 7s
184300K .......... .......... .......... .......... .......... 69% 18.6M 7s
184350K .......... .......... .......... .......... .......... 69% 22.5M 7s
184400K .......... .......... .......... .......... .......... 69% 16.7M 7s
184450K .......... .......... .......... .......... .......... 69% 18.7M 7s
184500K .......... .......... .......... .......... .......... 69% 19.7M 7s
184550K .......... .......... .......... .......... .......... 69% 17.8M 7s
184600K .......... .......... .......... .......... .......... 69% 19.3M 7s
184650K .......... .......... .......... .......... .......... 69% 19.2M 7s
184700K .......... .......... .......... .......... .......... 69% 19.4M 7s
184750K .......... .......... .......... .......... .......... 69% 20.0M 7s
184800K .......... .......... .......... .......... .......... 69% 23.7M 7s
184850K .......... .......... .......... .......... .......... 69% 14.3M 7s
184900K .......... .......... .......... .......... .......... 69% 23.2M 7s
184950K .......... .......... .......... .......... .......... 69% 30.2M 7s
185000K .......... .......... .......... .......... .......... 69% 10.5M 7s
185050K .......... .......... .......... .......... .......... 69% 43.2M 7s
185100K .......... .......... .......... .......... .......... 69% 13.0M 7s
185150K .......... .......... .......... .......... .......... 69% 25.5M 7s
185200K .......... .......... .......... .......... .......... 69% 20.2M 7s
185250K .......... .......... .......... .......... .......... 69% 18.0M 7s
185300K .......... .......... .......... .......... .......... 69% 16.7M 7s
185350K .......... .......... .......... .......... .......... 69% 17.5M 7s
185400K .......... .......... .......... .......... .......... 69% 29.1M 7s
185450K .......... .......... .......... .......... .......... 69% 11.8M 7s
185500K .......... .......... .......... .......... .......... 69% 28.5M 7s
185550K .......... .......... .......... .......... .......... 69% 12.6M 7s
185600K .......... .......... .......... .......... .......... 69% 24.7M 7s
185650K .......... .......... .......... .......... .......... 69% 17.2M 7s
185700K .......... .......... .......... .......... .......... 69% 15.6M 7s
185750K .......... .......... .......... .......... .......... 69% 28.2M 7s
185800K .......... .......... .......... .......... .......... 69% 18.8M 7s
185850K .......... .......... .......... .......... .......... 69% 10.8M 7s
185900K .......... .......... .......... .......... .......... 69% 38.8M 7s
185950K .......... .......... .......... .......... .......... 69% 19.5M 7s
186000K .......... .......... .......... .......... .......... 70% 15.0M 7s
186050K .......... .......... .......... .......... .......... 70% 20.1M 7s
186100K .......... .......... .......... .......... .......... 70% 15.8M 7s
186150K .......... .......... .......... .......... .......... 70% 19.1M 7s
186200K .......... .......... .......... .......... .......... 70% 16.0M 7s
186250K .......... .......... .......... .......... .......... 70% 17.4M 7s
186300K .......... .......... .......... .......... .......... 70% 24.9M 7s
186350K .......... .......... .......... .......... .......... 70% 18.1M 7s
186400K .......... .......... .......... .......... .......... 70% 15.5M 7s
186450K .......... .......... .......... .......... .......... 70% 24.2M 7s
186500K .......... .......... .......... .......... .......... 70% 18.4M 7s
186550K .......... .......... .......... .......... .......... 70% 15.1M 7s
186600K .......... .......... .......... .......... .......... 70% 15.6M 7s
186650K .......... .......... .......... .......... .......... 70% 18.8M 7s
186700K .......... .......... .......... .......... .......... 70% 15.5M 7s
186750K .......... .......... .......... .......... .......... 70% 18.7M 7s
186800K .......... .......... .......... .......... .......... 70% 14.8M 7s
186850K .......... .......... .......... .......... .......... 70% 16.2M 7s
186900K .......... .......... .......... .......... .......... 70% 16.9M 7s
186950K .......... .......... .......... .......... .......... 70% 26.4M 7s
187000K .......... .......... .......... .......... .......... 70% 19.6M 7s
187050K .......... .......... .......... .......... .......... 70% 19.9M 7s
187100K .......... .......... .......... .......... .......... 70% 13.6M 7s
187150K .......... .......... .......... .......... .......... 70% 18.8M 7s
187200K .......... .......... .......... .......... .......... 70% 5.18M 7s
187250K .......... .......... .......... .......... .......... 70% 88.3M 7s
187300K .......... .......... .......... .......... .......... 70% 61.6M 7s
187350K .......... .......... .......... .......... .......... 70% 39.7M 7s
187400K .......... .......... .......... .......... .......... 70% 14.7M 7s
187450K .......... .......... .......... .......... .......... 70% 16.9M 7s
187500K .......... .......... .......... .......... .......... 70% 15.8M 7s
187550K .......... .......... .......... .......... .......... 70% 10.7M 7s
187600K .......... .......... .......... .......... .......... 70% 18.2M 7s
187650K .......... .......... .......... .......... .......... 70% 12.1M 7s
187700K .......... .......... .......... .......... .......... 70% 11.5M 7s
187750K .......... .......... .......... .......... .......... 70% 31.0M 7s
187800K .......... .......... .......... .......... .......... 70% 12.1M 7s
187850K .......... .......... .......... .......... .......... 70% 23.0M 7s
187900K .......... .......... .......... .......... .......... 70% 9.99M 7s
187950K .......... .......... .......... .......... .......... 70% 6.04M 7s
188000K .......... .......... .......... .......... .......... 70% 94.9M 7s
188050K .......... .......... .......... .......... .......... 70% 63.3M 7s
188100K .......... .......... .......... .......... .......... 70% 22.1M 7s
188150K .......... .......... .......... .......... .......... 70% 11.4M 7s
188200K .......... .......... .......... .......... .......... 70% 11.8M 7s
188250K .......... .......... .......... .......... .......... 70% 13.3M 7s
188300K .......... .......... .......... .......... .......... 70% 19.4M 7s
188350K .......... .......... .......... .......... .......... 70% 10.9M 7s
188400K .......... .......... .......... .......... .......... 70% 14.7M 7s
188450K .......... .......... .......... .......... .......... 70% 10.6M 7s
188500K .......... .......... .......... .......... .......... 70% 12.9M 7s
188550K .......... .......... .......... .......... .......... 70% 15.8M 7s
188600K .......... .......... .......... .......... .......... 70% 18.0M 7s
188650K .......... .......... .......... .......... .......... 71% 11.9M 7s
188700K .......... .......... .......... .......... .......... 71% 10.2M 7s
188750K .......... .......... .......... .......... .......... 71% 17.5M 7s
188800K .......... .......... .......... .......... .......... 71% 16.5M 7s
188850K .......... .......... .......... .......... .......... 71% 10.8M 7s
188900K .......... .......... .......... .......... .......... 71% 10.5M 7s
188950K .......... .......... .......... .......... .......... 71% 29.4M 7s
189000K .......... .......... .......... .......... .......... 71% 10.1M 7s
189050K .......... .......... .......... .......... .......... 71% 13.6M 7s
189100K .......... .......... .......... .......... .......... 71% 11.0M 7s
189150K .......... .......... .......... .......... .......... 71% 17.5M 7s
189200K .......... .......... .......... .......... .......... 71% 5.79M 7s
189250K .......... .......... .......... .......... .......... 71% 103M 7s
189300K .......... .......... .......... .......... .......... 71% 12.0M 7s
189350K .......... .......... .......... .......... .......... 71% 12.1M 7s
189400K .......... .......... .......... .......... .......... 71% 12.6M 7s
189450K .......... .......... .......... .......... .......... 71% 11.7M 7s
189500K .......... .......... .......... .......... .......... 71% 13.9M 7s
189550K .......... .......... .......... .......... .......... 71% 13.4M 7s
189600K .......... .......... .......... .......... .......... 71% 11.7M 7s
189650K .......... .......... .......... .......... .......... 71% 13.0M 7s
189700K .......... .......... .......... .......... .......... 71% 12.5M 7s
189750K .......... .......... .......... .......... .......... 71% 12.1M 7s
189800K .......... .......... .......... .......... .......... 71% 11.3M 7s
189850K .......... .......... .......... .......... .......... 71% 12.0M 7s
189900K .......... .......... .......... .......... .......... 71% 13.2M 7s
189950K .......... .......... .......... .......... .......... 71% 9.52M 7s
190000K .......... .......... .......... .......... .......... 71% 13.6M 7s
190050K .......... .......... .......... .......... .......... 71% 19.5M 7s
190100K .......... .......... .......... .......... .......... 71% 14.1M 7s
190150K .......... .......... .......... .......... .......... 71% 9.35M 7s
190200K .......... .......... .......... .......... .......... 71% 97.2M 7s
190250K .......... .......... .......... .......... .......... 71% 19.6M 7s
190300K .......... .......... .......... .......... .......... 71% 15.4M 7s
190350K .......... .......... .......... .......... .......... 71% 9.04M 7s
190400K .......... .......... .......... .......... .......... 71% 17.1M 7s
190450K .......... .......... .......... .......... .......... 71% 12.1M 7s
190500K .......... .......... .......... .......... .......... 71% 10.4M 7s
190550K .......... .......... .......... .......... .......... 71% 17.3M 7s
190600K .......... .......... .......... .......... .......... 71% 13.8M 7s
190650K .......... .......... .......... .......... .......... 71% 10.9M 7s
190700K .......... .......... .......... .......... .......... 71% 14.8M 7s
190750K .......... .......... .......... .......... .......... 71% 19.6M 7s
190800K .......... .......... .......... .......... .......... 71% 14.0M 7s
190850K .......... .......... .......... .......... .......... 71% 14.1M 7s
190900K .......... .......... .......... .......... .......... 71% 17.5M 7s
190950K .......... .......... .......... .......... .......... 71% 16.1M 7s
191000K .......... .......... .......... .......... .......... 71% 10.0M 7s
191050K .......... .......... .......... .......... .......... 71% 79.8M 7s
191100K .......... .......... .......... .......... .......... 71% 16.0M 7s
191150K .......... .......... .......... .......... .......... 71% 26.1M 7s
191200K .......... .......... .......... .......... .......... 71% 12.4M 7s
191250K .......... .......... .......... .......... .......... 71% 16.4M 6s
191300K .......... .......... .......... .......... .......... 72% 15.2M 6s
191350K .......... .......... .......... .......... .......... 72% 16.3M 6s
191400K .......... .......... .......... .......... .......... 72% 18.3M 6s
191450K .......... .......... .......... .......... .......... 72% 12.5M 6s
191500K .......... .......... .......... .......... .......... 72% 22.1M 6s
191550K .......... .......... .......... .......... .......... 72% 18.2M 6s
191600K .......... .......... .......... .......... .......... 72% 17.9M 6s
191650K .......... .......... .......... .......... .......... 72% 27.2M 6s
191700K .......... .......... .......... .......... .......... 72% 16.7M 6s
191750K .......... .......... .......... .......... .......... 72% 15.1M 6s
191800K .......... .......... .......... .......... .......... 72% 15.9M 6s
191850K .......... .......... .......... .......... .......... 72% 21.4M 6s
191900K .......... .......... .......... .......... .......... 72% 17.7M 6s
191950K .......... .......... .......... .......... .......... 72% 18.3M 6s
192000K .......... .......... .......... .......... .......... 72% 17.1M 6s
192050K .......... .......... .......... .......... .......... 72% 96.9M 6s
192100K .......... .......... .......... .......... .......... 72% 16.0M 6s
192150K .......... .......... .......... .......... .......... 72% 19.5M 6s
192200K .......... .......... .......... .......... .......... 72% 18.5M 6s
192250K .......... .......... .......... .......... .......... 72% 9.01M 6s
192300K .......... .......... .......... .......... .......... 72% 94.8M 6s
192350K .......... .......... .......... .......... .......... 72% 25.9M 6s
192400K .......... .......... .......... .......... .......... 72% 35.9M 6s
192450K .......... .......... .......... .......... .......... 72% 14.1M 6s
192500K .......... .......... .......... .......... .......... 72% 16.7M 6s
192550K .......... .......... .......... .......... .......... 72% 18.6M 6s
192600K .......... .......... .......... .......... .......... 72% 15.6M 6s
192650K .......... .......... .......... .......... .......... 72% 18.6M 6s
192700K .......... .......... .......... .......... .......... 72% 14.2M 6s
192750K .......... .......... .......... .......... .......... 72% 16.6M 6s
192800K .......... .......... .......... .......... .......... 72% 18.0M 6s
192850K .......... .......... .......... .......... .......... 72% 13.2M 6s
192900K .......... .......... .......... .......... .......... 72% 16.4M 6s
192950K .......... .......... .......... .......... .......... 72% 17.3M 6s
193000K .......... .......... .......... .......... .......... 72% 16.9M 6s
193050K .......... .......... .......... .......... .......... 72% 17.7M 6s
193100K .......... .......... .......... .......... .......... 72% 16.0M 6s
193150K .......... .......... .......... .......... .......... 72% 50.4M 6s
193200K .......... .......... .......... .......... .......... 72% 14.5M 6s
193250K .......... .......... .......... .......... .......... 72% 18.5M 6s
193300K .......... .......... .......... .......... .......... 72% 16.4M 6s
193350K .......... .......... .......... .......... .......... 72% 12.6M 6s
193400K .......... .......... .......... .......... .......... 72% 16.1M 6s
193450K .......... .......... .......... .......... .......... 72% 22.2M 6s
193500K .......... .......... .......... .......... .......... 72% 14.4M 6s
193550K .......... .......... .......... .......... .......... 72% 21.6M 6s
193600K .......... .......... .......... .......... .......... 72% 6.34M 6s
193650K .......... .......... .......... .......... .......... 72% 140M 6s
193700K .......... .......... .......... .......... .......... 72% 34.1M 6s
193750K .......... .......... .......... .......... .......... 72% 15.3M 6s
193800K .......... .......... .......... .......... .......... 72% 12.9M 6s
193850K .......... .......... .......... .......... .......... 72% 14.1M 6s
193900K .......... .......... .......... .......... .......... 72% 13.3M 6s
193950K .......... .......... .......... .......... .......... 73% 12.8M 6s
194000K .......... .......... .......... .......... .......... 73% 20.1M 6s
194050K .......... .......... .......... .......... .......... 73% 16.9M 6s
194100K .......... .......... .......... .......... .......... 73% 10.0M 6s
194150K .......... .......... .......... .......... .......... 73% 16.9M 6s
194200K .......... .......... .......... .......... .......... 73% 14.6M 6s
194250K .......... .......... .......... .......... .......... 73% 8.04M 6s
194300K .......... .......... .......... .......... .......... 73% 80.6M 6s
194350K .......... .......... .......... .......... .......... 73% 25.5M 6s
194400K .......... .......... .......... .......... .......... 73% 16.6M 6s
194450K .......... .......... .......... .......... .......... 73% 7.85M 6s
194500K .......... .......... .......... .......... .......... 73% 23.5M 6s
194550K .......... .......... .......... .......... .......... 73% 15.6M 6s
194600K .......... .......... .......... .......... .......... 73% 10.5M 6s
194650K .......... .......... .......... .......... .......... 73% 16.7M 6s
194700K .......... .......... .......... .......... .......... 73% 15.4M 6s
194750K .......... .......... .......... .......... .......... 73% 19.9M 6s
194800K .......... .......... .......... .......... .......... 73% 11.5M 6s
194850K .......... .......... .......... .......... .......... 73% 15.2M 6s
194900K .......... .......... .......... .......... .......... 73% 17.0M 6s
194950K .......... .......... .......... .......... .......... 73% 17.0M 6s
195000K .......... .......... .......... .......... .......... 73% 18.1M 6s
195050K .......... .......... .......... .......... .......... 73% 14.3M 6s
195100K .......... .......... .......... .......... .......... 73% 19.9M 6s
195150K .......... .......... .......... .......... .......... 73% 16.0M 6s
195200K .......... .......... .......... .......... .......... 73% 16.5M 6s
195250K .......... .......... .......... .......... .......... 73% 17.3M 6s
195300K .......... .......... .......... .......... .......... 73% 17.7M 6s
195350K .......... .......... .......... .......... .......... 73% 17.5M 6s
195400K .......... .......... .......... .......... .......... 73% 17.3M 6s
195450K .......... .......... .......... .......... .......... 73% 15.6M 6s
195500K .......... .......... .......... .......... .......... 73% 18.1M 6s
195550K .......... .......... .......... .......... .......... 73% 16.2M 6s
195600K .......... .......... .......... .......... .......... 73% 15.3M 6s
195650K .......... .......... .......... .......... .......... 73% 16.6M 6s
195700K .......... .......... .......... .......... .......... 73% 17.1M 6s
195750K .......... .......... .......... .......... .......... 73% 15.3M 6s
195800K .......... .......... .......... .......... .......... 73% 84.1M 6s
195850K .......... .......... .......... .......... .......... 73% 16.0M 6s
195900K .......... .......... .......... .......... .......... 73% 10.0M 6s
195950K .......... .......... .......... .......... .......... 73% 15.9M 6s
196000K .......... .......... .......... .......... .......... 73% 30.9M 6s
196050K .......... .......... .......... .......... .......... 73% 14.6M 6s
196100K .......... .......... .......... .......... .......... 73% 14.7M 6s
196150K .......... .......... .......... .......... .......... 73% 19.7M 6s
196200K .......... .......... .......... .......... .......... 73% 14.3M 6s
196250K .......... .......... .......... .......... .......... 73% 90.5M 6s
196300K .......... .......... .......... .......... .......... 73% 17.2M 6s
196350K .......... .......... .......... .......... .......... 73% 13.6M 6s
196400K .......... .......... .......... .......... .......... 73% 15.7M 6s
196450K .......... .......... .......... .......... .......... 73% 15.0M 6s
196500K .......... .......... .......... .......... .......... 73% 51.0M 6s
196550K .......... .......... .......... .......... .......... 73% 13.1M 6s
196600K .......... .......... .......... .......... .......... 73% 14.6M 6s
196650K .......... .......... .......... .......... .......... 74% 13.8M 6s
196700K .......... .......... .......... .......... .......... 74% 16.4M 6s
196750K .......... .......... .......... .......... .......... 74% 38.8M 6s
196800K .......... .......... .......... .......... .......... 74% 16.4M 6s
196850K .......... .......... .......... .......... .......... 74% 14.2M 6s
196900K .......... .......... .......... .......... .......... 74% 23.1M 6s
196950K .......... .......... .......... .......... .......... 74% 15.3M 6s
197000K .......... .......... .......... .......... .......... 74% 23.5M 6s
197050K .......... .......... .......... .......... .......... 74% 18.6M 6s
197100K .......... .......... .......... .......... .......... 74% 13.6M 6s
197150K .......... .......... .......... .......... .......... 74% 32.0M 6s
197200K .......... .......... .......... .......... .......... 74% 22.0M 6s
197250K .......... .......... .......... .......... .......... 74% 15.6M 6s
197300K .......... .......... .......... .......... .......... 74% 17.1M 6s
197350K .......... .......... .......... .......... .......... 74% 15.2M 6s
197400K .......... .......... .......... .......... .......... 74% 21.4M 6s
197450K .......... .......... .......... .......... .......... 74% 17.3M 6s
197500K .......... .......... .......... .......... .......... 74% 15.5M 6s
197550K .......... .......... .......... .......... .......... 74% 20.7M 6s
197600K .......... .......... .......... .......... .......... 74% 13.4M 6s
197650K .......... .......... .......... .......... .......... 74% 10.1M 6s
197700K .......... .......... .......... .......... .......... 74% 21.9M 6s
197750K .......... .......... .......... .......... .......... 74% 10.4M 6s
197800K .......... .......... .......... .......... .......... 74% 13.5M 6s
197850K .......... .......... .......... .......... .......... 74% 14.6M 6s
197900K .......... .......... .......... .......... .......... 74% 13.4M 6s
197950K .......... .......... .......... .......... .......... 74% 11.1M 6s
198000K .......... .......... .......... .......... .......... 74% 13.6M 6s
198050K .......... .......... .......... .......... .......... 74% 17.4M 6s
198100K .......... .......... .......... .......... .......... 74% 12.2M 6s
198150K .......... .......... .......... .......... .......... 74% 12.0M 6s
198200K .......... .......... .......... .......... .......... 74% 37.7M 6s
198250K .......... .......... .......... .......... .......... 74% 14.4M 6s
198300K .......... .......... .......... .......... .......... 74% 20.4M 6s
198350K .......... .......... .......... .......... .......... 74% 15.7M 6s
198400K .......... .......... .......... .......... .......... 74% 17.3M 6s
198450K .......... .......... .......... .......... .......... 74% 10.1M 6s
198500K .......... .......... .......... .......... .......... 74% 19.5M 6s
198550K .......... .......... .......... .......... .......... 74% 13.9M 6s
198600K .......... .......... .......... .......... .......... 74% 16.7M 6s
198650K .......... .......... .......... .......... .......... 74% 12.4M 6s
198700K .......... .......... .......... .......... .......... 74% 14.0M 6s
198750K .......... .......... .......... .......... .......... 74% 16.7M 6s
198800K .......... .......... .......... .......... .......... 74% 11.9M 6s
198850K .......... .......... .......... .......... .......... 74% 26.3M 6s
198900K .......... .......... .......... .......... .......... 74% 9.27M 6s
198950K .......... .......... .......... .......... .......... 74% 10.7M 6s
199000K .......... .......... .......... .......... .......... 74% 23.4M 6s
199050K .......... .......... .......... .......... .......... 74% 9.96M 6s
199100K .......... .......... .......... .......... .......... 74% 17.3M 6s
199150K .......... .......... .......... .......... .......... 74% 20.7M 6s
199200K .......... .......... .......... .......... .......... 74% 15.3M 6s
199250K .......... .......... .......... .......... .......... 74% 29.3M 6s
199300K .......... .......... .......... .......... .......... 75% 17.3M 6s
199350K .......... .......... .......... .......... .......... 75% 22.6M 6s
199400K .......... .......... .......... .......... .......... 75% 12.7M 6s
199450K .......... .......... .......... .......... .......... 75% 18.9M 6s
199500K .......... .......... .......... .......... .......... 75% 23.1M 6s
199550K .......... .......... .......... .......... .......... 75% 20.0M 6s
199600K .......... .......... .......... .......... .......... 75% 18.6M 6s
199650K .......... .......... .......... .......... .......... 75% 12.6M 6s
199700K .......... .......... .......... .......... .......... 75% 18.8M 6s
199750K .......... .......... .......... .......... .......... 75% 17.7M 6s
199800K .......... .......... .......... .......... .......... 75% 22.4M 6s
199850K .......... .......... .......... .......... .......... 75% 19.4M 6s
199900K .......... .......... .......... .......... .......... 75% 13.1M 6s
199950K .......... .......... .......... .......... .......... 75% 42.4M 6s
200000K .......... .......... .......... .......... .......... 75% 10.8M 6s
200050K .......... .......... .......... .......... .......... 75% 22.8M 6s
200100K .......... .......... .......... .......... .......... 75% 18.7M 6s
200150K .......... .......... .......... .......... .......... 75% 19.4M 6s
200200K .......... .......... .......... .......... .......... 75% 19.1M 6s
200250K .......... .......... .......... .......... .......... 75% 12.5M 6s
200300K .......... .......... .......... .......... .......... 75% 30.3M 6s
200350K .......... .......... .......... .......... .......... 75% 13.1M 6s
200400K .......... .......... .......... .......... .......... 75% 39.8M 6s
200450K .......... .......... .......... .......... .......... 75% 11.7M 6s
200500K .......... .......... .......... .......... .......... 75% 22.3M 6s
200550K .......... .......... .......... .......... .......... 75% 18.4M 6s
200600K .......... .......... .......... .......... .......... 75% 11.6M 6s
200650K .......... .......... .......... .......... .......... 75% 34.3M 6s
200700K .......... .......... .......... .......... .......... 75% 11.8M 6s
200750K .......... .......... .......... .......... .......... 75% 38.0M 6s
200800K .......... .......... .......... .......... .......... 75% 13.6M 6s
200850K .......... .......... .......... .......... .......... 75% 18.2M 6s
200900K .......... .......... .......... .......... .......... 75% 19.9M 6s
200950K .......... .......... .......... .......... .......... 75% 17.6M 6s
201000K .......... .......... .......... .......... .......... 75% 25.6M 6s
201050K .......... .......... .......... .......... .......... 75% 15.7M 6s
201100K .......... .......... .......... .......... .......... 75% 17.1M 6s
201150K .......... .......... .......... .......... .......... 75% 21.9M 6s
201200K .......... .......... .......... .......... .......... 75% 18.1M 6s
201250K .......... .......... .......... .......... .......... 75% 22.3M 6s
201300K .......... .......... .......... .......... .......... 75% 20.1M 6s
201350K .......... .......... .......... .......... .......... 75% 9.98M 6s
201400K .......... .......... .......... .......... .......... 75% 51.5M 6s
201450K .......... .......... .......... .......... .......... 75% 13.9M 6s
201500K .......... .......... .......... .......... .......... 75% 23.4M 6s
201550K .......... .......... .......... .......... .......... 75% 16.2M 6s
201600K .......... .......... .......... .......... .......... 75% 17.3M 6s
201650K .......... .......... .......... .......... .......... 75% 19.3M 5s
201700K .......... .......... .......... .......... .......... 75% 20.4M 5s
201750K .......... .......... .......... .......... .......... 75% 44.5M 5s
201800K .......... .......... .......... .......... .......... 75% 11.3M 5s
201850K .......... .......... .......... .......... .......... 75% 38.0M 5s
201900K .......... .......... .......... .......... .......... 75% 19.1M 5s
201950K .......... .......... .......... .......... .......... 76% 17.9M 5s
202000K .......... .......... .......... .......... .......... 76% 13.3M 5s
202050K .......... .......... .......... .......... .......... 76% 33.2M 5s
202100K .......... .......... .......... .......... .......... 76% 12.3M 5s
202150K .......... .......... .......... .......... .......... 76% 44.6M 5s
202200K .......... .......... .......... .......... .......... 76% 10.4M 5s
202250K .......... .......... .......... .......... .......... 76% 30.3M 5s
202300K .......... .......... .......... .......... .......... 76% 13.9M 5s
202350K .......... .......... .......... .......... .......... 76% 26.7M 5s
202400K .......... .......... .......... .......... .......... 76% 24.2M 5s
202450K .......... .......... .......... .......... .......... 76% 14.2M 5s
202500K .......... .......... .......... .......... .......... 76% 55.7M 5s
202550K .......... .......... .......... .......... .......... 76% 11.4M 5s
202600K .......... .......... .......... .......... .......... 76% 42.2M 5s
202650K .......... .......... .......... .......... .......... 76% 11.8M 5s
202700K .......... .......... .......... .......... .......... 76% 70.2M 5s
202750K .......... .......... .......... .......... .......... 76% 10.1M 5s
202800K .......... .......... .......... .......... .......... 76% 41.6M 5s
202850K .......... .......... .......... .......... .......... 76% 11.1M 5s
202900K .......... .......... .......... .......... .......... 76% 50.1M 5s
202950K .......... .......... .......... .......... .......... 76% 25.3M 5s
203000K .......... .......... .......... .......... .......... 76% 13.3M 5s
203050K .......... .......... .......... .......... .......... 76% 28.3M 5s
203100K .......... .......... .......... .......... .......... 76% 12.4M 5s
203150K .......... .......... .......... .......... .......... 76% 68.5M 5s
203200K .......... .......... .......... .......... .......... 76% 10.1M 5s
203250K .......... .......... .......... .......... .......... 76% 59.9M 5s
203300K .......... .......... .......... .......... .......... 76% 10.9M 5s
203350K .......... .......... .......... .......... .......... 76% 45.8M 5s
203400K .......... .......... .......... .......... .......... 76% 20.9M 5s
203450K .......... .......... .......... .......... .......... 76% 15.2M 5s
203500K .......... .......... .......... .......... .......... 76% 20.0M 5s
203550K .......... .......... .......... .......... .......... 76% 16.3M 5s
203600K .......... .......... .......... .......... .......... 76% 17.1M 5s
203650K .......... .......... .......... .......... .......... 76% 16.9M 5s
203700K .......... .......... .......... .......... .......... 76% 17.4M 5s
203750K .......... .......... .......... .......... .......... 76% 19.0M 5s
203800K .......... .......... .......... .......... .......... 76% 23.1M 5s
203850K .......... .......... .......... .......... .......... 76% 14.1M 5s
203900K .......... .......... .......... .......... .......... 76% 21.5M 5s
203950K .......... .......... .......... .......... .......... 76% 14.8M 5s
204000K .......... .......... .......... .......... .......... 76% 23.6M 5s
204050K .......... .......... .......... .......... .......... 76% 31.3M 5s
204100K .......... .......... .......... .......... .......... 76% 19.2M 5s
204150K .......... .......... .......... .......... .......... 76% 23.7M 5s
204200K .......... .......... .......... .......... .......... 76% 17.2M 5s
204250K .......... .......... .......... .......... .......... 76% 6.32M 5s
204300K .......... .......... .......... .......... .......... 76% 64.0M 5s
204350K .......... .......... .......... .......... .......... 76% 65.8M 5s
204400K .......... .......... .......... .......... .......... 76% 52.5M 5s
204450K .......... .......... .......... .......... .......... 76% 45.4M 5s
204500K .......... .......... .......... .......... .......... 76% 12.2M 5s
204550K .......... .......... .......... .......... .......... 76% 18.6M 5s
204600K .......... .......... .......... .......... .......... 77% 15.9M 5s
204650K .......... .......... .......... .......... .......... 77% 12.9M 5s
204700K .......... .......... .......... .......... .......... 77% 35.1M 5s
204750K .......... .......... .......... .......... .......... 77% 12.8M 5s
204800K .......... .......... .......... .......... .......... 77% 16.0M 5s
204850K .......... .......... .......... .......... .......... 77% 16.0M 5s
204900K .......... .......... .......... .......... .......... 77% 15.5M 5s
204950K .......... .......... .......... .......... .......... 77% 26.7M 5s
205000K .......... .......... .......... .......... .......... 77% 11.2M 5s
205050K .......... .......... .......... .......... .......... 77% 55.4M 5s
205100K .......... .......... .......... .......... .......... 77% 5.21M 5s
205150K .......... .......... .......... .......... .......... 77% 75.6M 5s
205200K .......... .......... .......... .......... .......... 77% 58.0M 5s
205250K .......... .......... .......... .......... .......... 77% 18.4M 5s
205300K .......... .......... .......... .......... .......... 77% 12.1M 5s
205350K .......... .......... .......... .......... .......... 77% 11.8M 5s
205400K .......... .......... .......... .......... .......... 77% 18.0M 5s
205450K .......... .......... .......... .......... .......... 77% 9.85M 5s
205500K .......... .......... .......... .......... .......... 77% 17.6M 5s
205550K .......... .......... .......... .......... .......... 77% 17.9M 5s
205600K .......... .......... .......... .......... .......... 77% 13.6M 5s
205650K .......... .......... .......... .......... .......... 77% 15.3M 5s
205700K .......... .......... .......... .......... .......... 77% 14.0M 5s
205750K .......... .......... .......... .......... .......... 77% 13.6M 5s
205800K .......... .......... .......... .......... .......... 77% 13.8M 5s
205850K .......... .......... .......... .......... .......... 77% 12.2M 5s
205900K .......... .......... .......... .......... .......... 77% 14.3M 5s
205950K .......... .......... .......... .......... .......... 77% 16.0M 5s
206000K .......... .......... .......... .......... .......... 77% 14.0M 5s
206050K .......... .......... .......... .......... .......... 77% 15.7M 5s
206100K .......... .......... .......... .......... .......... 77% 11.9M 5s
206150K .......... .......... .......... .......... .......... 77% 18.6M 5s
206200K .......... .......... .......... .......... .......... 77% 6.78M 5s
206250K .......... .......... .......... .......... .......... 77% 23.8M 5s
206300K .......... .......... .......... .......... .......... 77% 24.2M 5s
206350K .......... .......... .......... .......... .......... 77% 10.9M 5s
206400K .......... .......... .......... .......... .......... 77% 14.4M 5s
206450K .......... .......... .......... .......... .......... 77% 10.1M 5s
206500K .......... .......... .......... .......... .......... 77% 14.9M 5s
206550K .......... .......... .......... .......... .......... 77% 12.9M 5s
206600K .......... .......... .......... .......... .......... 77% 13.2M 5s
206650K .......... .......... .......... .......... .......... 77% 9.86M 5s
206700K .......... .......... .......... .......... .......... 77% 11.2M 5s
206750K .......... .......... .......... .......... .......... 77% 17.8M 5s
206800K .......... .......... .......... .......... .......... 77% 20.5M 5s
206850K .......... .......... .......... .......... .......... 77% 9.55M 5s
206900K .......... .......... .......... .......... .......... 77% 13.3M 5s
206950K .......... .......... .......... .......... .......... 77% 13.6M 5s
207000K .......... .......... .......... .......... .......... 77% 13.4M 5s
207050K .......... .......... .......... .......... .......... 77% 13.4M 5s
207100K .......... .......... .......... .......... .......... 77% 14.1M 5s
207150K .......... .......... .......... .......... .......... 77% 16.3M 5s
207200K .......... .......... .......... .......... .......... 77% 6.44M 5s
207250K .......... .......... .......... .......... .......... 78% 110M 5s
207300K .......... .......... .......... .......... .......... 78% 14.3M 5s
207350K .......... .......... .......... .......... .......... 78% 10.7M 5s
207400K .......... .......... .......... .......... .......... 78% 17.7M 5s
207450K .......... .......... .......... .......... .......... 78% 11.3M 5s
207500K .......... .......... .......... .......... .......... 78% 16.4M 5s
207550K .......... .......... .......... .......... .......... 78% 12.3M 5s
207600K .......... .......... .......... .......... .......... 78% 11.5M 5s
207650K .......... .......... .......... .......... .......... 78% 14.3M 5s
207700K .......... .......... .......... .......... .......... 78% 15.4M 5s
207750K .......... .......... .......... .......... .......... 78% 11.5M 5s
207800K .......... .......... .......... .......... .......... 78% 14.1M 5s
207850K .......... .......... .......... .......... .......... 78% 13.4M 5s
207900K .......... .......... .......... .......... .......... 78% 16.1M 5s
207950K .......... .......... .......... .......... .......... 78% 14.2M 5s
208000K .......... .......... .......... .......... .......... 78% 15.0M 5s
208050K .......... .......... .......... .......... .......... 78% 15.8M 5s
208100K .......... .......... .......... .......... .......... 78% 16.5M 5s
208150K .......... .......... .......... .......... .......... 78% 14.7M 5s
208200K .......... .......... .......... .......... .......... 78% 10.5M 5s
208250K .......... .......... .......... .......... .......... 78% 7.48M 5s
208300K .......... .......... .......... .......... .......... 78% 164M 5s
208350K .......... .......... .......... .......... .......... 78% 14.8M 5s
208400K .......... .......... .......... .......... .......... 78% 14.2M 5s
208450K .......... .......... .......... .......... .......... 78% 8.07M 5s
208500K .......... .......... .......... .......... .......... 78% 15.9M 5s
208550K .......... .......... .......... .......... .......... 78% 15.0M 5s
208600K .......... .......... .......... .......... .......... 78% 11.2M 5s
208650K .......... .......... .......... .......... .......... 78% 10.4M 5s
208700K .......... .......... .......... .......... .......... 78% 10.3M 5s
208750K .......... .......... .......... .......... .......... 78% 12.8M 5s
208800K .......... .......... .......... .......... .......... 78% 13.9M 5s
208850K .......... .......... .......... .......... .......... 78% 10.2M 5s
208900K .......... .......... .......... .......... .......... 78% 11.1M 5s
208950K .......... .......... .......... .......... .......... 78% 14.9M 5s
209000K .......... .......... .......... .......... .......... 78% 15.6M 5s
209050K .......... .......... .......... .......... .......... 78% 16.1M 5s
209100K .......... .......... .......... .......... .......... 78% 14.9M 5s
209150K .......... .......... .......... .......... .......... 78% 16.0M 5s
209200K .......... .......... .......... .......... .......... 78% 12.9M 5s
209250K .......... .......... .......... .......... .......... 78% 15.5M 5s
209300K .......... .......... .......... .......... .......... 78% 14.4M 5s
209350K .......... .......... .......... .......... .......... 78% 15.3M 5s
209400K .......... .......... .......... .......... .......... 78% 13.6M 5s
209450K .......... .......... .......... .......... .......... 78% 13.3M 5s
209500K .......... .......... .......... .......... .......... 78% 14.7M 5s
209550K .......... .......... .......... .......... .......... 78% 15.0M 5s
209600K .......... .......... .......... .......... .......... 78% 14.6M 5s
209650K .......... .......... .......... .......... .......... 78% 12.8M 5s
209700K .......... .......... .......... .......... .......... 78% 13.6M 5s
209750K .......... .......... .......... .......... .......... 78% 16.7M 5s
209800K .......... .......... .......... .......... .......... 78% 14.4M 5s
209850K .......... .......... .......... .......... .......... 78% 15.9M 5s
209900K .......... .......... .......... .......... .......... 79% 15.6M 5s
209950K .......... .......... .......... .......... .......... 79% 15.6M 5s
210000K .......... .......... .......... .......... .......... 79% 18.5M 5s
210050K .......... .......... .......... .......... .......... 79% 15.1M 5s
210100K .......... .......... .......... .......... .......... 79% 15.4M 5s
210150K .......... .......... .......... .......... .......... 79% 16.3M 5s
210200K .......... .......... .......... .......... .......... 79% 16.2M 5s
210250K .......... .......... .......... .......... .......... 79% 19.5M 5s
210300K .......... .......... .......... .......... .......... 79% 15.1M 5s
210350K .......... .......... .......... .......... .......... 79% 15.5M 5s
210400K .......... .......... .......... .......... .......... 79% 14.6M 5s
210450K .......... .......... .......... .......... .......... 79% 20.9M 5s
210500K .......... .......... .......... .......... .......... 79% 46.7M 5s
210550K .......... .......... .......... .......... .......... 79% 14.2M 5s
210600K .......... .......... .......... .......... .......... 79% 15.4M 5s
210650K .......... .......... .......... .......... .......... 79% 70.2M 5s
210700K .......... .......... .......... .......... .......... 79% 16.1M 5s
210750K .......... .......... .......... .......... .......... 79% 13.0M 5s
210800K .......... .......... .......... .......... .......... 79% 13.9M 5s
210850K .......... .......... .......... .......... .......... 79% 49.2M 5s
210900K .......... .......... .......... .......... .......... 79% 15.9M 5s
210950K .......... .......... .......... .......... .......... 79% 13.4M 5s
211000K .......... .......... .......... .......... .......... 79% 15.0M 5s
211050K .......... .......... .......... .......... .......... 79% 95.2M 5s
211100K .......... .......... .......... .......... .......... 79% 13.3M 5s
211150K .......... .......... .......... .......... .......... 79% 19.6M 5s
211200K .......... .......... .......... .......... .......... 79% 29.7M 5s
211250K .......... .......... .......... .......... .......... 79% 13.7M 5s
211300K .......... .......... .......... .......... .......... 79% 19.7M 5s
211350K .......... .......... .......... .......... .......... 79% 19.5M 5s
211400K .......... .......... .......... .......... .......... 79% 15.1M 5s
211450K .......... .......... .......... .......... .......... 79% 15.3M 5s
211500K .......... .......... .......... .......... .......... 79% 22.2M 5s
211550K .......... .......... .......... .......... .......... 79% 24.4M 5s
211600K .......... .......... .......... .......... .......... 79% 13.0M 5s
211650K .......... .......... .......... .......... .......... 79% 16.8M 5s
211700K .......... .......... .......... .......... .......... 79% 23.0M 5s
211750K .......... .......... .......... .......... .......... 79% 18.6M 5s
211800K .......... .......... .......... .......... .......... 79% 17.2M 5s
211850K .......... .......... .......... .......... .......... 79% 14.0M 5s
211900K .......... .......... .......... .......... .......... 79% 18.8M 5s
211950K .......... .......... .......... .......... .......... 79% 13.8M 5s
212000K .......... .......... .......... .......... .......... 79% 18.7M 5s
212050K .......... .......... .......... .......... .......... 79% 41.2M 5s
212100K .......... .......... .......... .......... .......... 79% 12.0M 5s
212150K .......... .......... .......... .......... .......... 79% 15.1M 5s
212200K .......... .......... .......... .......... .......... 79% 24.6M 5s
212250K .......... .......... .......... .......... .......... 79% 14.3M 5s
212300K .......... .......... .......... .......... .......... 79% 35.9M 5s
212350K .......... .......... .......... .......... .......... 79% 13.1M 5s
212400K .......... .......... .......... .......... .......... 79% 14.4M 5s
212450K .......... .......... .......... .......... .......... 79% 17.4M 5s
212500K .......... .......... .......... .......... .......... 79% 29.9M 4s
212550K .......... .......... .......... .......... .......... 80% 18.2M 4s
212600K .......... .......... .......... .......... .......... 80% 22.3M 4s
212650K .......... .......... .......... .......... .......... 80% 16.1M 4s
212700K .......... .......... .......... .......... .......... 80% 11.7M 4s
212750K .......... .......... .......... .......... .......... 80% 100M 4s
212800K .......... .......... .......... .......... .......... 80% 14.6M 4s
212850K .......... .......... .......... .......... .......... 80% 37.5M 4s
212900K .......... .......... .......... .......... .......... 80% 20.8M 4s
212950K .......... .......... .......... .......... .......... 80% 13.4M 4s
213000K .......... .......... .......... .......... .......... 80% 35.0M 4s
213050K .......... .......... .......... .......... .......... 80% 14.1M 4s
213100K .......... .......... .......... .......... .......... 80% 26.0M 4s
213150K .......... .......... .......... .......... .......... 80% 16.4M 4s
213200K .......... .......... .......... .......... .......... 80% 15.6M 4s
213250K .......... .......... .......... .......... .......... 80% 27.8M 4s
213300K .......... .......... .......... .......... .......... 80% 15.8M 4s
213350K .......... .......... .......... .......... .......... 80% 30.7M 4s
213400K .......... .......... .......... .......... .......... 80% 17.4M 4s
213450K .......... .......... .......... .......... .......... 80% 14.9M 4s
213500K .......... .......... .......... .......... .......... 80% 28.4M 4s
213550K .......... .......... .......... .......... .......... 80% 23.0M 4s
213600K .......... .......... .......... .......... .......... 80% 15.3M 4s
213650K .......... .......... .......... .......... .......... 80% 8.08M 4s
213700K .......... .......... .......... .......... .......... 80% 53.3M 4s
213750K .......... .......... .......... .......... .......... 80% 55.8M 4s
213800K .......... .......... .......... .......... .......... 80% 11.8M 4s
213850K .......... .......... .......... .......... .......... 80% 13.0M 4s
213900K .......... .......... .......... .......... .......... 80% 11.7M 4s
213950K .......... .......... .......... .......... .......... 80% 21.6M 4s
214000K .......... .......... .......... .......... .......... 80% 12.6M 4s
214050K .......... .......... .......... .......... .......... 80% 5.53M 4s
214100K .......... .......... .......... .......... .......... 80% 44.2M 4s
214150K .......... .......... .......... .......... .......... 80% 39.0M 4s
214200K .......... .......... .......... .......... .......... 80% 12.7M 4s
214250K .......... .......... .......... .......... .......... 80% 13.6M 4s
214300K .......... .......... .......... .......... .......... 80% 11.2M 4s
214350K .......... .......... .......... .......... .......... 80% 15.4M 4s
214400K .......... .......... .......... .......... .......... 80% 13.7M 4s
214450K .......... .......... .......... .......... .......... 80% 14.4M 4s
214500K .......... .......... .......... .......... .......... 80% 13.6M 4s
214550K .......... .......... .......... .......... .......... 80% 9.90M 4s
214600K .......... .......... .......... .......... .......... 80% 13.1M 4s
214650K .......... .......... .......... .......... .......... 80% 14.8M 4s
214700K .......... .......... .......... .......... .......... 80% 11.7M 4s
214750K .......... .......... .......... .......... .......... 80% 23.2M 4s
214800K .......... .......... .......... .......... .......... 80% 14.8M 4s
214850K .......... .......... .......... .......... .......... 80% 9.64M 4s
214900K .......... .......... .......... .......... .......... 80% 32.7M 4s
214950K .......... .......... .......... .......... .......... 80% 12.2M 4s
215000K .......... .......... .......... .......... .......... 80% 13.9M 4s
215050K .......... .......... .......... .......... .......... 80% 16.1M 4s
215100K .......... .......... .......... .......... .......... 80% 10.7M 4s
215150K .......... .......... .......... .......... .......... 80% 14.7M 4s
215200K .......... .......... .......... .......... .......... 80% 15.6M 4s
215250K .......... .......... .......... .......... .......... 81% 28.1M 4s
215300K .......... .......... .......... .......... .......... 81% 13.3M 4s
215350K .......... .......... .......... .......... .......... 81% 7.43M 4s
215400K .......... .......... .......... .......... .......... 81% 52.3M 4s
215450K .......... .......... .......... .......... .......... 81% 10.8M 4s
215500K .......... .......... .......... .......... .......... 81% 16.9M 4s
215550K .......... .......... .......... .......... .......... 81% 14.2M 4s
215600K .......... .......... .......... .......... .......... 81% 12.3M 4s
215650K .......... .......... .......... .......... .......... 81% 10.8M 4s
215700K .......... .......... .......... .......... .......... 81% 14.5M 4s
215750K .......... .......... .......... .......... .......... 81% 15.0M 4s
215800K .......... .......... .......... .......... .......... 81% 18.1M 4s
215850K .......... .......... .......... .......... .......... 81% 18.1M 4s
215900K .......... .......... .......... .......... .......... 81% 18.8M 4s
215950K .......... .......... .......... .......... .......... 81% 9.82M 4s
216000K .......... .......... .......... .......... .......... 81% 16.2M 4s
216050K .......... .......... .......... .......... .......... 81% 17.5M 4s
216100K .......... .......... .......... .......... .......... 81% 17.0M 4s
216150K .......... .......... .......... .......... .......... 81% 11.9M 4s
216200K .......... .......... .......... .......... .......... 81% 30.8M 4s
216250K .......... .......... .......... .......... .......... 81% 16.7M 4s
216300K .......... .......... .......... .......... .......... 81% 32.0M 4s
216350K .......... .......... .......... .......... .......... 81% 12.7M 4s
216400K .......... .......... .......... .......... .......... 81% 16.9M 4s
216450K .......... .......... .......... .......... .......... 81% 20.8M 4s
216500K .......... .......... .......... .......... .......... 81% 14.8M 4s
216550K .......... .......... .......... .......... .......... 81% 22.2M 4s
216600K .......... .......... .......... .......... .......... 81% 17.0M 4s
216650K .......... .......... .......... .......... .......... 81% 123M 4s
216700K .......... .......... .......... .......... .......... 81% 15.3M 4s
216750K .......... .......... .......... .......... .......... 81% 15.3M 4s
216800K .......... .......... .......... .......... .......... 81% 20.6M 4s
216850K .......... .......... .......... .......... .......... 81% 18.0M 4s
216900K .......... .......... .......... .......... .......... 81% 17.2M 4s
216950K .......... .......... .......... .......... .......... 81% 19.0M 4s
217000K .......... .......... .......... .......... .......... 81% 17.8M 4s
217050K .......... .......... .......... .......... .......... 81% 19.5M 4s
217100K .......... .......... .......... .......... .......... 81% 17.4M 4s
217150K .......... .......... .......... .......... .......... 81% 49.0M 4s
217200K .......... .......... .......... .......... .......... 81% 12.3M 4s
217250K .......... .......... .......... .......... .......... 81% 30.4M 4s
217300K .......... .......... .......... .......... .......... 81% 33.2M 4s
217350K .......... .......... .......... .......... .......... 81% 16.3M 4s
217400K .......... .......... .......... .......... .......... 81% 19.4M 4s
217450K .......... .......... .......... .......... .......... 81% 22.8M 4s
217500K .......... .......... .......... .......... .......... 81% 34.8M 4s
217550K .......... .......... .......... .......... .......... 81% 17.3M 4s
217600K .......... .......... .......... .......... .......... 81% 19.6M 4s
217650K .......... .......... .......... .......... .......... 81% 22.3M 4s
217700K .......... .......... .......... .......... .......... 81% 39.3M 4s
217750K .......... .......... .......... .......... .......... 81% 19.5M 4s
217800K .......... .......... .......... .......... .......... 81% 20.7M 4s
217850K .......... .......... .......... .......... .......... 81% 33.7M 4s
217900K .......... .......... .......... .......... .......... 82% 17.0M 4s
217950K .......... .......... .......... .......... .......... 82% 17.7M 4s
218000K .......... .......... .......... .......... .......... 82% 60.3M 4s
218050K .......... .......... .......... .......... .......... 82% 25.6M 4s
218100K .......... .......... .......... .......... .......... 82% 15.5M 4s
218150K .......... .......... .......... .......... .......... 82% 81.1M 4s
218200K .......... .......... .......... .......... .......... 82% 18.7M 4s
218250K .......... .......... .......... .......... .......... 82% 24.5M 4s
218300K .......... .......... .......... .......... .......... 82% 58.8M 4s
218350K .......... .......... .......... .......... .......... 82% 19.8M 4s
218400K .......... .......... .......... .......... .......... 82% 16.7M 4s
218450K .......... .......... .......... .......... .......... 82% 79.5M 4s
218500K .......... .......... .......... .......... .......... 82% 22.3M 4s
218550K .......... .......... .......... .......... .......... 82% 19.0M 4s
218600K .......... .......... .......... .......... .......... 82% 35.5M 4s
218650K .......... .......... .......... .......... .......... 82% 23.0M 4s
218700K .......... .......... .......... .......... .......... 82% 18.7M 4s
218750K .......... .......... .......... .......... .......... 82% 20.1M 4s
218800K .......... .......... .......... .......... .......... 82% 39.0M 4s
218850K .......... .......... .......... .......... .......... 82% 19.4M 4s
218900K .......... .......... .......... .......... .......... 82% 25.8M 4s
218950K .......... .......... .......... .......... .......... 82% 33.3M 4s
219000K .......... .......... .......... .......... .......... 82% 21.9M 4s
219050K .......... .......... .......... .......... .......... 82% 24.5M 4s
219100K .......... .......... .......... .......... .......... 82% 18.8M 4s
219150K .......... .......... .......... .......... .......... 82% 32.1M 4s
219200K .......... .......... .......... .......... .......... 82% 21.0M 4s
219250K .......... .......... .......... .......... .......... 82% 9.97M 4s
219300K .......... .......... .......... .......... .......... 82% 153M 4s
219350K .......... .......... .......... .......... .......... 82% 142M 4s
219400K .......... .......... .......... .......... .......... 82% 91.3M 4s
219450K .......... .......... .......... .......... .......... 82% 15.4M 4s
219500K .......... .......... .......... .......... .......... 82% 25.0M 4s
219550K .......... .......... .......... .......... .......... 82% 16.2M 4s
219600K .......... .......... .......... .......... .......... 82% 25.4M 4s
219650K .......... .......... .......... .......... .......... 82% 19.9M 4s
219700K .......... .......... .......... .......... .......... 82% 22.7M 4s
219750K .......... .......... .......... .......... .......... 82% 21.0M 4s
219800K .......... .......... .......... .......... .......... 82% 20.8M 4s
219850K .......... .......... .......... .......... .......... 82% 19.4M 4s
219900K .......... .......... .......... .......... .......... 82% 41.5M 4s
219950K .......... .......... .......... .......... .......... 82% 16.7M 4s
220000K .......... .......... .......... .......... .......... 82% 18.8M 4s
220050K .......... .......... .......... .......... .......... 82% 17.7M 4s
220100K .......... .......... .......... .......... .......... 82% 16.4M 4s
220150K .......... .......... .......... .......... .......... 82% 15.8M 4s
220200K .......... .......... .......... .......... .......... 82% 16.4M 4s
220250K .......... .......... .......... .......... .......... 82% 41.4M 4s
220300K .......... .......... .......... .......... .......... 82% 25.9M 4s
220350K .......... .......... .......... .......... .......... 82% 16.4M 4s
220400K .......... .......... .......... .......... .......... 82% 19.5M 4s
220450K .......... .......... .......... .......... .......... 82% 38.1M 4s
220500K .......... .......... .......... .......... .......... 82% 16.6M 4s
220550K .......... .......... .......... .......... .......... 83% 17.5M 4s
220600K .......... .......... .......... .......... .......... 83% 20.9M 4s
220650K .......... .......... .......... .......... .......... 83% 43.3M 4s
220700K .......... .......... .......... .......... .......... 83% 14.9M 4s
220750K .......... .......... .......... .......... .......... 83% 16.5M 4s
220800K .......... .......... .......... .......... .......... 83% 71.5M 4s
220850K .......... .......... .......... .......... .......... 83% 13.0M 4s
220900K .......... .......... .......... .......... .......... 83% 18.6M 4s
220950K .......... .......... .......... .......... .......... 83% 17.3M 4s
221000K .......... .......... .......... .......... .......... 83% 47.6M 4s
221050K .......... .......... .......... .......... .......... 83% 15.9M 4s
221100K .......... .......... .......... .......... .......... 83% 18.7M 4s
221150K .......... .......... .......... .......... .......... 83% 19.7M 4s
221200K .......... .......... .......... .......... .......... 83% 18.4M 4s
221250K .......... .......... .......... .......... .......... 83% 29.1M 4s
221300K .......... .......... .......... .......... .......... 83% 15.0M 4s
221350K .......... .......... .......... .......... .......... 83% 16.6M 4s
221400K .......... .......... .......... .......... .......... 83% 22.1M 4s
221450K .......... .......... .......... .......... .......... 83% 41.9M 4s
221500K .......... .......... .......... .......... .......... 83% 13.4M 4s
221550K .......... .......... .......... .......... .......... 83% 29.5M 4s
221600K .......... .......... .......... .......... .......... 83% 15.1M 4s
221650K .......... .......... .......... .......... .......... 83% 26.1M 4s
221700K .......... .......... .......... .......... .......... 83% 16.2M 4s
221750K .......... .......... .......... .......... .......... 83% 22.2M 4s
221800K .......... .......... .......... .......... .......... 83% 34.2M 4s
221850K .......... .......... .......... .......... .......... 83% 13.6M 4s
221900K .......... .......... .......... .......... .......... 83% 19.2M 4s
221950K .......... .......... .......... .......... .......... 83% 27.6M 4s
222000K .......... .......... .......... .......... .......... 83% 25.3M 4s
222050K .......... .......... .......... .......... .......... 83% 19.8M 4s
222100K .......... .......... .......... .......... .......... 83% 20.3M 4s
222150K .......... .......... .......... .......... .......... 83% 16.5M 4s
222200K .......... .......... .......... .......... .......... 83% 23.8M 4s
222250K .......... .......... .......... .......... .......... 83% 16.6M 4s
222300K .......... .......... .......... .......... .......... 83% 19.6M 4s
222350K .......... .......... .......... .......... .......... 83% 12.8M 4s
222400K .......... .......... .......... .......... .......... 83% 27.1M 4s
222450K .......... .......... .......... .......... .......... 83% 15.5M 4s
222500K .......... .......... .......... .......... .......... 83% 46.2M 4s
222550K .......... .......... .......... .......... .......... 83% 16.2M 4s
222600K .......... .......... .......... .......... .......... 83% 20.5M 4s
222650K .......... .......... .......... .......... .......... 83% 20.8M 4s
222700K .......... .......... .......... .......... .......... 83% 18.9M 4s
222750K .......... .......... .......... .......... .......... 83% 29.0M 4s
222800K .......... .......... .......... .......... .......... 83% 14.5M 4s
222850K .......... .......... .......... .......... .......... 83% 30.8M 4s
222900K .......... .......... .......... .......... .......... 83% 17.4M 4s
222950K .......... .......... .......... .......... .......... 83% 21.9M 4s
223000K .......... .......... .......... .......... .......... 83% 23.9M 4s
223050K .......... .......... .......... .......... .......... 83% 25.3M 4s
223100K .......... .......... .......... .......... .......... 83% 13.8M 4s
223150K .......... .......... .......... .......... .......... 83% 31.8M 4s
223200K .......... .......... .......... .......... .......... 84% 17.5M 4s
223250K .......... .......... .......... .......... .......... 84% 22.3M 4s
223300K .......... .......... .......... .......... .......... 84% 24.8M 4s
223350K .......... .......... .......... .......... .......... 84% 14.8M 4s
223400K .......... .......... .......... .......... .......... 84% 72.2M 4s
223450K .......... .......... .......... .......... .......... 84% 13.2M 4s
223500K .......... .......... .......... .......... .......... 84% 69.9M 4s
223550K .......... .......... .......... .......... .......... 84% 14.5M 3s
223600K .......... .......... .......... .......... .......... 84% 71.4M 3s
223650K .......... .......... .......... .......... .......... 84% 15.1M 3s
223700K .......... .......... .......... .......... .......... 84% 44.7M 3s
223750K .......... .......... .......... .......... .......... 84% 25.1M 3s
223800K .......... .......... .......... .......... .......... 84% 26.3M 3s
223850K .......... .......... .......... .......... .......... 84% 23.5M 3s
223900K .......... .......... .......... .......... .......... 84% 34.2M 3s
223950K .......... .......... .......... .......... .......... 84% 17.2M 3s
224000K .......... .......... .......... .......... .......... 84% 83.5M 3s
224050K .......... .......... .......... .......... .......... 84% 17.4M 3s
224100K .......... .......... .......... .......... .......... 84% 57.7M 3s
224150K .......... .......... .......... .......... .......... 84% 20.6M 3s
224200K .......... .......... .......... .......... .......... 84% 41.3M 3s
224250K .......... .......... .......... .......... .......... 84% 18.2M 3s
224300K .......... .......... .......... .......... .......... 84% 51.1M 3s
224350K .......... .......... .......... .......... .......... 84% 19.1M 3s
224400K .......... .......... .......... .......... .......... 84% 21.5M 3s
224450K .......... .......... .......... .......... .......... 84% 32.3M 3s
224500K .......... .......... .......... .......... .......... 84% 24.9M 3s
224550K .......... .......... .......... .......... .......... 84% 34.1M 3s
224600K .......... .......... .......... .......... .......... 84% 22.3M 3s
224650K .......... .......... .......... .......... .......... 84% 27.6M 3s
224700K .......... .......... .......... .......... .......... 84% 15.6M 3s
224750K .......... .......... .......... .......... .......... 84% 48.1M 3s
224800K .......... .......... .......... .......... .......... 84% 14.3M 3s
224850K .......... .......... .......... .......... .......... 84% 63.5M 3s
224900K .......... .......... .......... .......... .......... 84% 17.8M 3s
224950K .......... .......... .......... .......... .......... 84% 56.1M 3s
225000K .......... .......... .......... .......... .......... 84% 16.9M 3s
225050K .......... .......... .......... .......... .......... 84% 80.7M 3s
225100K .......... .......... .......... .......... .......... 84% 14.9M 3s
225150K .......... .......... .......... .......... .......... 84% 59.7M 3s
225200K .......... .......... .......... .......... .......... 84% 48.0M 3s
225250K .......... .......... .......... .......... .......... 84% 19.6M 3s
225300K .......... .......... .......... .......... .......... 84% 51.3M 3s
225350K .......... .......... .......... .......... .......... 84% 17.8M 3s
225400K .......... .......... .......... .......... .......... 84% 44.8M 3s
225450K .......... .......... .......... .......... .......... 84% 15.7M 3s
225500K .......... .......... .......... .......... .......... 84% 46.2M 3s
225550K .......... .......... .......... .......... .......... 84% 8.10M 3s
225600K .......... .......... .......... .......... .......... 84% 74.6M 3s
225650K .......... .......... .......... .......... .......... 84% 64.0M 3s
225700K .......... .......... .......... .......... .......... 84% 12.5M 3s
225750K .......... .......... .......... .......... .......... 84% 83.1M 3s
225800K .......... .......... .......... .......... .......... 84% 61.0M 3s
225850K .......... .......... .......... .......... .......... 85% 19.9M 3s
225900K .......... .......... .......... .......... .......... 85% 18.1M 3s
225950K .......... .......... .......... .......... .......... 85% 17.3M 3s
226000K .......... .......... .......... .......... .......... 85% 20.3M 3s
226050K .......... .......... .......... .......... .......... 85% 19.0M 3s
226100K .......... .......... .......... .......... .......... 85% 18.7M 3s
226150K .......... .......... .......... .......... .......... 85% 18.6M 3s
226200K .......... .......... .......... .......... .......... 85% 17.8M 3s
226250K .......... .......... .......... .......... .......... 85% 13.2M 3s
226300K .......... .......... .......... .......... .......... 85% 17.6M 3s
226350K .......... .......... .......... .......... .......... 85% 11.9M 3s
226400K .......... .......... .......... .......... .......... 85% 31.1M 3s
226450K .......... .......... .......... .......... .......... 85% 20.8M 3s
226500K .......... .......... .......... .......... .......... 85% 17.6M 3s
226550K .......... .......... .......... .......... .......... 85% 15.4M 3s
226600K .......... .......... .......... .......... .......... 85% 17.3M 3s
226650K .......... .......... .......... .......... .......... 85% 90.3M 3s
226700K .......... .......... .......... .......... .......... 85% 16.4M 3s
226750K .......... .......... .......... .......... .......... 85% 19.5M 3s
226800K .......... .......... .......... .......... .......... 85% 17.6M 3s
226850K .......... .......... .......... .......... .......... 85% 14.5M 3s
226900K .......... .......... .......... .......... .......... 85% 97.1M 3s
226950K .......... .......... .......... .......... .......... 85% 18.3M 3s
227000K .......... .......... .......... .......... .......... 85% 8.47M 3s
227050K .......... .......... .......... .......... .......... 85% 16.9M 3s
227100K .......... .......... .......... .......... .......... 85% 26.9M 3s
227150K .......... .......... .......... .......... .......... 85% 15.5M 3s
227200K .......... .......... .......... .......... .......... 85% 18.8M 3s
227250K .......... .......... .......... .......... .......... 85% 24.4M 3s
227300K .......... .......... .......... .......... .......... 85% 33.2M 3s
227350K .......... .......... .......... .......... .......... 85% 13.7M 3s
227400K .......... .......... .......... .......... .......... 85% 16.7M 3s
227450K .......... .......... .......... .......... .......... 85% 22.3M 3s
227500K .......... .......... .......... .......... .......... 85% 22.7M 3s
227550K .......... .......... .......... .......... .......... 85% 17.9M 3s
227600K .......... .......... .......... .......... .......... 85% 25.6M 3s
227650K .......... .......... .......... .......... .......... 85% 22.3M 3s
227700K .......... .......... .......... .......... .......... 85% 14.4M 3s
227750K .......... .......... .......... .......... .......... 85% 14.6M 3s
227800K .......... .......... .......... .......... .......... 85% 21.5M 3s
227850K .......... .......... .......... .......... .......... 85% 18.1M 3s
227900K .......... .......... .......... .......... .......... 85% 118M 3s
227950K .......... .......... .......... .......... .......... 85% 25.9M 3s
228000K .......... .......... .......... .......... .......... 85% 20.6M 3s
228050K .......... .......... .......... .......... .......... 85% 16.7M 3s
228100K .......... .......... .......... .......... .......... 85% 11.7M 3s
228150K .......... .......... .......... .......... .......... 85% 137M 3s
228200K .......... .......... .......... .......... .......... 85% 13.8M 3s
228250K .......... .......... .......... .......... .......... 85% 31.7M 3s
228300K .......... .......... .......... .......... .......... 85% 19.5M 3s
228350K .......... .......... .......... .......... .......... 85% 12.5M 3s
228400K .......... .......... .......... .......... .......... 85% 17.5M 3s
228450K .......... .......... .......... .......... .......... 85% 13.6M 3s
228500K .......... .......... .......... .......... .......... 86% 19.5M 3s
228550K .......... .......... .......... .......... .......... 86% 19.2M 3s
228600K .......... .......... .......... .......... .......... 86% 12.5M 3s
228650K .......... .......... .......... .......... .......... 86% 28.0M 3s
228700K .......... .......... .......... .......... .......... 86% 13.6M 3s
228750K .......... .......... .......... .......... .......... 86% 18.1M 3s
228800K .......... .......... .......... .......... .......... 86% 18.8M 3s
228850K .......... .......... .......... .......... .......... 86% 20.5M 3s
228900K .......... .......... .......... .......... .......... 86% 21.1M 3s
228950K .......... .......... .......... .......... .......... 86% 23.6M 3s
229000K .......... .......... .......... .......... .......... 86% 14.8M 3s
229050K .......... .......... .......... .......... .......... 86% 18.0M 3s
229100K .......... .......... .......... .......... .......... 86% 30.0M 3s
229150K .......... .......... .......... .......... .......... 86% 20.0M 3s
229200K .......... .......... .......... .......... .......... 86% 19.2M 3s
229250K .......... .......... .......... .......... .......... 86% 13.0M 3s
229300K .......... .......... .......... .......... .......... 86% 18.2M 3s
229350K .......... .......... .......... .......... .......... 86% 26.9M 3s
229400K .......... .......... .......... .......... .......... 86% 12.9M 3s
229450K .......... .......... .......... .......... .......... 86% 16.1M 3s
229500K .......... .......... .......... .......... .......... 86% 20.6M 3s
229550K .......... .......... .......... .......... .......... 86% 18.6M 3s
229600K .......... .......... .......... .......... .......... 86% 13.9M 3s
229650K .......... .......... .......... .......... .......... 86% 21.2M 3s
229700K .......... .......... .......... .......... .......... 86% 15.3M 3s
229750K .......... .......... .......... .......... .......... 86% 111M 3s
229800K .......... .......... .......... .......... .......... 86% 13.6M 3s
229850K .......... .......... .......... .......... .......... 86% 17.8M 3s
229900K .......... .......... .......... .......... .......... 86% 45.2M 3s
229950K .......... .......... .......... .......... .......... 86% 20.2M 3s
230000K .......... .......... .......... .......... .......... 86% 16.6M 3s
230050K .......... .......... .......... .......... .......... 86% 17.2M 3s
230100K .......... .......... .......... .......... .......... 86% 17.8M 3s
230150K .......... .......... .......... .......... .......... 86% 39.8M 3s
230200K .......... .......... .......... .......... .......... 86% 16.9M 3s
230250K .......... .......... .......... .......... .......... 86% 15.1M 3s
230300K .......... .......... .......... .......... .......... 86% 41.9M 3s
230350K .......... .......... .......... .......... .......... 86% 17.3M 3s
230400K .......... .......... .......... .......... .......... 86% 14.8M 3s
230450K .......... .......... .......... .......... .......... 86% 32.1M 3s
230500K .......... .......... .......... .......... .......... 86% 14.1M 3s
230550K .......... .......... .......... .......... .......... 86% 32.9M 3s
230600K .......... .......... .......... .......... .......... 86% 16.2M 3s
230650K .......... .......... .......... .......... .......... 86% 14.6M 3s
230700K .......... .......... .......... .......... .......... 86% 25.6M 3s
230750K .......... .......... .......... .......... .......... 86% 26.6M 3s
230800K .......... .......... .......... .......... .......... 86% 15.8M 3s
230850K .......... .......... .......... .......... .......... 86% 15.1M 3s
230900K .......... .......... .......... .......... .......... 86% 40.1M 3s
230950K .......... .......... .......... .......... .......... 86% 14.8M 3s
231000K .......... .......... .......... .......... .......... 86% 18.1M 3s
231050K .......... .......... .......... .......... .......... 86% 42.8M 3s
231100K .......... .......... .......... .......... .......... 86% 14.3M 3s
231150K .......... .......... .......... .......... .......... 87% 19.5M 3s
231200K .......... .......... .......... .......... .......... 87% 16.6M 3s
231250K .......... .......... .......... .......... .......... 87% 27.9M 3s
231300K .......... .......... .......... .......... .......... 87% 14.5M 3s
231350K .......... .......... .......... .......... .......... 87% 31.7M 3s
231400K .......... .......... .......... .......... .......... 87% 16.0M 3s
231450K .......... .......... .......... .......... .......... 87% 15.8M 3s
231500K .......... .......... .......... .......... .......... 87% 24.2M 3s
231550K .......... .......... .......... .......... .......... 87% 19.3M 3s
231600K .......... .......... .......... .......... .......... 87% 12.8M 3s
231650K .......... .......... .......... .......... .......... 87% 52.8M 3s
231700K .......... .......... .......... .......... .......... 87% 17.1M 3s
231750K .......... .......... .......... .......... .......... 87% 40.3M 3s
231800K .......... .......... .......... .......... .......... 87% 14.8M 3s
231850K .......... .......... .......... .......... .......... 87% 14.3M 3s
231900K .......... .......... .......... .......... .......... 87% 56.5M 3s
231950K .......... .......... .......... .......... .......... 87% 14.8M 3s
232000K .......... .......... .......... .......... .......... 87% 33.0M 3s
232050K .......... .......... .......... .......... .......... 87% 15.7M 3s
232100K .......... .......... .......... .......... .......... 87% 19.2M 3s
232150K .......... .......... .......... .......... .......... 87% 17.5M 3s
232200K .......... .......... .......... .......... .......... 87% 24.9M 3s
232250K .......... .......... .......... .......... .......... 87% 16.7M 3s
232300K .......... .......... .......... .......... .......... 87% 23.5M 3s
232350K .......... .......... .......... .......... .......... 87% 18.9M 3s
232400K .......... .......... .......... .......... .......... 87% 19.7M 3s
232450K .......... .......... .......... .......... .......... 87% 14.4M 3s
232500K .......... .......... .......... .......... .......... 87% 19.6M 3s
232550K .......... .......... .......... .......... .......... 87% 19.5M 3s
232600K .......... .......... .......... .......... .......... 87% 11.2M 3s
232650K .......... .......... .......... .......... .......... 87% 18.7M 3s
232700K .......... .......... .......... .......... .......... 87% 17.7M 3s
232750K .......... .......... .......... .......... .......... 87% 16.3M 3s
232800K .......... .......... .......... .......... .......... 87% 35.7M 3s
232850K .......... .......... .......... .......... .......... 87% 15.4M 3s
232900K .......... .......... .......... .......... .......... 87% 22.1M 3s
232950K .......... .......... .......... .......... .......... 87% 17.0M 3s
233000K .......... .......... .......... .......... .......... 87% 25.1M 3s
233050K .......... .......... .......... .......... .......... 87% 18.4M 3s
233100K .......... .......... .......... .......... .......... 87% 25.4M 3s
233150K .......... .......... .......... .......... .......... 87% 12.6M 3s
233200K .......... .......... .......... .......... .......... 87% 22.0M 3s
233250K .......... .......... .......... .......... .......... 87% 17.3M 3s
233300K .......... .......... .......... .......... .......... 87% 28.7M 3s
233350K .......... .......... .......... .......... .......... 87% 15.2M 3s
233400K .......... .......... .......... .......... .......... 87% 30.6M 3s
233450K .......... .......... .......... .......... .......... 87% 13.3M 3s
233500K .......... .......... .......... .......... .......... 87% 31.7M 3s
233550K .......... .......... .......... .......... .......... 87% 15.7M 3s
233600K .......... .......... .......... .......... .......... 87% 16.2M 3s
233650K .......... .......... .......... .......... .......... 87% 22.7M 3s
233700K .......... .......... .......... .......... .......... 87% 12.9M 3s
233750K .......... .......... .......... .......... .......... 87% 25.5M 3s
233800K .......... .......... .......... .......... .......... 87% 18.0M 3s
233850K .......... .......... .......... .......... .......... 88% 16.0M 3s
233900K .......... .......... .......... .......... .......... 88% 20.1M 3s
233950K .......... .......... .......... .......... .......... 88% 18.7M 3s
234000K .......... .......... .......... .......... .......... 88% 18.9M 3s
234050K .......... .......... .......... .......... .......... 88% 80.1M 3s
234100K .......... .......... .......... .......... .......... 88% 13.3M 3s
234150K .......... .......... .......... .......... .......... 88% 17.7M 3s
234200K .......... .......... .......... .......... .......... 88% 19.8M 3s
234250K .......... .......... .......... .......... .......... 88% 20.1M 3s
234300K .......... .......... .......... .......... .......... 88% 24.9M 3s
234350K .......... .......... .......... .......... .......... 88% 15.8M 3s
234400K .......... .......... .......... .......... .......... 88% 20.5M 3s
234450K .......... .......... .......... .......... .......... 88% 20.7M 3s
234500K .......... .......... .......... .......... .......... 88% 18.7M 3s
234550K .......... .......... .......... .......... .......... 88% 21.9M 3s
234600K .......... .......... .......... .......... .......... 88% 19.0M 3s
234650K .......... .......... .......... .......... .......... 88% 14.6M 3s
234700K .......... .......... .......... .......... .......... 88% 29.0M 3s
234750K .......... .......... .......... .......... .......... 88% 18.5M 3s
234800K .......... .......... .......... .......... .......... 88% 11.5M 3s
234850K .......... .......... .......... .......... .......... 88% 58.3M 3s
234900K .......... .......... .......... .......... .......... 88% 36.2M 3s
234950K .......... .......... .......... .......... .......... 88% 16.4M 3s
235000K .......... .......... .......... .......... .......... 88% 26.4M 2s
235050K .......... .......... .......... .......... .......... 88% 16.8M 2s
235100K .......... .......... .......... .......... .......... 88% 21.8M 2s
235150K .......... .......... .......... .......... .......... 88% 17.0M 2s
235200K .......... .......... .......... .......... .......... 88% 19.1M 2s
235250K .......... .......... .......... .......... .......... 88% 18.9M 2s
235300K .......... .......... .......... .......... .......... 88% 32.5M 2s
235350K .......... .......... .......... .......... .......... 88% 14.8M 2s
235400K .......... .......... .......... .......... .......... 88% 26.2M 2s
235450K .......... .......... .......... .......... .......... 88% 16.5M 2s
235500K .......... .......... .......... .......... .......... 88% 22.2M 2s
235550K .......... .......... .......... .......... .......... 88% 27.3M 2s
235600K .......... .......... .......... .......... .......... 88% 14.6M 2s
235650K .......... .......... .......... .......... .......... 88% 26.0M 2s
235700K .......... .......... .......... .......... .......... 88% 21.3M 2s
235750K .......... .......... .......... .......... .......... 88% 54.8M 2s
235800K .......... .......... .......... .......... .......... 88% 11.4M 2s
235850K .......... .......... .......... .......... .......... 88% 33.0M 2s
235900K .......... .......... .......... .......... .......... 88% 15.0M 2s
235950K .......... .......... .......... .......... .......... 88% 25.6M 2s
236000K .......... .......... .......... .......... .......... 88% 14.4M 2s
236050K .......... .......... .......... .......... .......... 88% 26.6M 2s
236100K .......... .......... .......... .......... .......... 88% 42.5M 2s
236150K .......... .......... .......... .......... .......... 88% 15.1M 2s
236200K .......... .......... .......... .......... .......... 88% 23.0M 2s
236250K .......... .......... .......... .......... .......... 88% 16.2M 2s
236300K .......... .......... .......... .......... .......... 88% 25.8M 2s
236350K .......... .......... .......... .......... .......... 88% 16.1M 2s
236400K .......... .......... .......... .......... .......... 88% 38.4M 2s
236450K .......... .......... .......... .......... .......... 88% 12.4M 2s
236500K .......... .......... .......... .......... .......... 89% 44.9M 2s
236550K .......... .......... .......... .......... .......... 89% 14.2M 2s
236600K .......... .......... .......... .......... .......... 89% 26.9M 2s
236650K .......... .......... .......... .......... .......... 89% 23.0M 2s
236700K .......... .......... .......... .......... .......... 89% 18.0M 2s
236750K .......... .......... .......... .......... .......... 89% 23.6M 2s
236800K .......... .......... .......... .......... .......... 89% 21.2M 2s
236850K .......... .......... .......... .......... .......... 89% 44.1M 2s
236900K .......... .......... .......... .......... .......... 89% 12.3M 2s
236950K .......... .......... .......... .......... .......... 89% 53.3M 2s
237000K .......... .......... .......... .......... .......... 89% 11.6M 2s
237050K .......... .......... .......... .......... .......... 89% 58.1M 2s
237100K .......... .......... .......... .......... .......... 89% 16.3M 2s
237150K .......... .......... .......... .......... .......... 89% 26.6M 2s
237200K .......... .......... .......... .......... .......... 89% 13.0M 2s
237250K .......... .......... .......... .......... .......... 89% 20.8M 2s
237300K .......... .......... .......... .......... .......... 89% 33.3M 2s
237350K .......... .......... .......... .......... .......... 89% 8.70M 2s
237400K .......... .......... .......... .......... .......... 89% 36.2M 2s
237450K .......... .......... .......... .......... .......... 89% 9.71M 2s
237500K .......... .......... .......... .......... .......... 89% 48.7M 2s
237550K .......... .......... .......... .......... .......... 89% 20.5M 2s
237600K .......... .......... .......... .......... .......... 89% 12.1M 2s
237650K .......... .......... .......... .......... .......... 89% 69.1M 2s
237700K .......... .......... .......... .......... .......... 89% 11.1M 2s
237750K .......... .......... .......... .......... .......... 89% 29.4M 2s
237800K .......... .......... .......... .......... .......... 89% 8.18M 2s
237850K .......... .......... .......... .......... .......... 89% 33.6M 2s
237900K .......... .......... .......... .......... .......... 89% 67.4M 2s
237950K .......... .......... .......... .......... .......... 89% 11.8M 2s
238000K .......... .......... .......... .......... .......... 89% 47.4M 2s
238050K .......... .......... .......... .......... .......... 89% 10.4M 2s
238100K .......... .......... .......... .......... .......... 89% 57.7M 2s
238150K .......... .......... .......... .......... .......... 89% 46.3M 2s
238200K .......... .......... .......... .......... .......... 89% 11.2M 2s
238250K .......... .......... .......... .......... .......... 89% 62.7M 2s
238300K .......... .......... .......... .......... .......... 89% 10.3M 2s
238350K .......... .......... .......... .......... .......... 89% 46.7M 2s
238400K .......... .......... .......... .......... .......... 89% 45.2M 2s
238450K .......... .......... .......... .......... .......... 89% 10.6M 2s
238500K .......... .......... .......... .......... .......... 89% 53.4M 2s
238550K .......... .......... .......... .......... .......... 89% 53.6M 2s
238600K .......... .......... .......... .......... .......... 89% 8.97M 2s
238650K .......... .......... .......... .......... .......... 89% 27.7M 2s
238700K .......... .......... .......... .......... .......... 89% 11.4M 2s
238750K .......... .......... .......... .......... .......... 89% 38.8M 2s
238800K .......... .......... .......... .......... .......... 89% 35.9M 2s
238850K .......... .......... .......... .......... .......... 89% 11.5M 2s
238900K .......... .......... .......... .......... .......... 89% 41.3M 2s
238950K .......... .......... .......... .......... .......... 89% 15.0M 2s
239000K .......... .......... .......... .......... .......... 89% 54.2M 2s
239050K .......... .......... .......... .......... .......... 89% 25.9M 2s
239100K .......... .......... .......... .......... .......... 89% 14.1M 2s
239150K .......... .......... .......... .......... .......... 90% 75.5M 2s
239200K .......... .......... .......... .......... .......... 90% 20.1M 2s
239250K .......... .......... .......... .......... .......... 90% 14.9M 2s
239300K .......... .......... .......... .......... .......... 90% 32.2M 2s
239350K .......... .......... .......... .......... .......... 90% 13.8M 2s
239400K .......... .......... .......... .......... .......... 90% 38.1M 2s
239450K .......... .......... .......... .......... .......... 90% 26.7M 2s
239500K .......... .......... .......... .......... .......... 90% 15.3M 2s
239550K .......... .......... .......... .......... .......... 90% 33.2M 2s
239600K .......... .......... .......... .......... .......... 90% 11.8M 2s
239650K .......... .......... .......... .......... .......... 90% 49.6M 2s
239700K .......... .......... .......... .......... .......... 90% 21.6M 2s
239750K .......... .......... .......... .......... .......... 90% 14.8M 2s
239800K .......... .......... .......... .......... .......... 90% 54.1M 2s
239850K .......... .......... .......... .......... .......... 90% 18.9M 2s
239900K .......... .......... .......... .......... .......... 90% 19.0M 2s
239950K .......... .......... .......... .......... .......... 90% 19.1M 2s
240000K .......... .......... .......... .......... .......... 90% 47.0M 2s
240050K .......... .......... .......... .......... .......... 90% 14.6M 2s
240100K .......... .......... .......... .......... .......... 90% 22.6M 2s
240150K .......... .......... .......... .......... .......... 90% 20.1M 2s
240200K .......... .......... .......... .......... .......... 90% 14.8M 2s
240250K .......... .......... .......... .......... .......... 90% 56.3M 2s
240300K .......... .......... .......... .......... .......... 90% 15.6M 2s
240350K .......... .......... .......... .......... .......... 90% 22.6M 2s
240400K .......... .......... .......... .......... .......... 90% 18.4M 2s
240450K .......... .......... .......... .......... .......... 90% 23.0M 2s
240500K .......... .......... .......... .......... .......... 90% 22.4M 2s
240550K .......... .......... .......... .......... .......... 90% 16.6M 2s
240600K .......... .......... .......... .......... .......... 90% 26.2M 2s
240650K .......... .......... .......... .......... .......... 90% 17.5M 2s
240700K .......... .......... .......... .......... .......... 90% 23.3M 2s
240750K .......... .......... .......... .......... .......... 90% 23.5M 2s
240800K .......... .......... .......... .......... .......... 90% 20.0M 2s
240850K .......... .......... .......... .......... .......... 90% 22.5M 2s
240900K .......... .......... .......... .......... .......... 90% 17.4M 2s
240950K .......... .......... .......... .......... .......... 90% 19.3M 2s
241000K .......... .......... .......... .......... .......... 90% 26.2M 2s
241050K .......... .......... .......... .......... .......... 90% 23.0M 2s
241100K .......... .......... .......... .......... .......... 90% 20.5M 2s
241150K .......... .......... .......... .......... .......... 90% 14.3M 2s
241200K .......... .......... .......... .......... .......... 90% 35.7M 2s
241250K .......... .......... .......... .......... .......... 90% 24.2M 2s
241300K .......... .......... .......... .......... .......... 90% 20.7M 2s
241350K .......... .......... .......... .......... .......... 90% 22.9M 2s
241400K .......... .......... .......... .......... .......... 90% 40.8M 2s
241450K .......... .......... .......... .......... .......... 90% 19.8M 2s
241500K .......... .......... .......... .......... .......... 90% 27.6M 2s
241550K .......... .......... .......... .......... .......... 90% 26.9M 2s
241600K .......... .......... .......... .......... .......... 90% 30.3M 2s
241650K .......... .......... .......... .......... .......... 90% 24.0M 2s
241700K .......... .......... .......... .......... .......... 90% 26.3M 2s
241750K .......... .......... .......... .......... .......... 90% 47.3M 2s
241800K .......... .......... .......... .......... .......... 91% 18.1M 2s
241850K .......... .......... .......... .......... .......... 91% 29.0M 2s
241900K .......... .......... .......... .......... .......... 91% 23.9M 2s
241950K .......... .......... .......... .......... .......... 91% 23.9M 2s
242000K .......... .......... .......... .......... .......... 91% 43.2M 2s
242050K .......... .......... .......... .......... .......... 91% 26.2M 2s
242100K .......... .......... .......... .......... .......... 91% 22.9M 2s
242150K .......... .......... .......... .......... .......... 91% 21.6M 2s
242200K .......... .......... .......... .......... .......... 91% 23.0M 2s
242250K .......... .......... .......... .......... .......... 91% 76.8M 2s
242300K .......... .......... .......... .......... .......... 91% 18.7M 2s
242350K .......... .......... .......... .......... .......... 91% 21.6M 2s
242400K .......... .......... .......... .......... .......... 91% 23.4M 2s
242450K .......... .......... .......... .......... .......... 91% 21.3M 2s
242500K .......... .......... .......... .......... .......... 91% 44.9M 2s
242550K .......... .......... .......... .......... .......... 91% 23.9M 2s
242600K .......... .......... .......... .......... .......... 91% 21.4M 2s
242650K .......... .......... .......... .......... .......... 91% 21.7M 2s
242700K .......... .......... .......... .......... .......... 91% 21.7M 2s
242750K .......... .......... .......... .......... .......... 91% 45.8M 2s
242800K .......... .......... .......... .......... .......... 91% 26.6M 2s
242850K .......... .......... .......... .......... .......... 91% 48.4M 2s
242900K .......... .......... .......... .......... .......... 91% 17.8M 2s
242950K .......... .......... .......... .......... .......... 91% 28.4M 2s
243000K .......... .......... .......... .......... .......... 91% 31.4M 2s
243050K .......... .......... .......... .......... .......... 91% 22.9M 2s
243100K .......... .......... .......... .......... .......... 91% 26.8M 2s
243150K .......... .......... .......... .......... .......... 91% 18.4M 2s
243200K .......... .......... .......... .......... .......... 91% 28.8M 2s
243250K .......... .......... .......... .......... .......... 91% 31.4M 2s
243300K .......... .......... .......... .......... .......... 91% 26.7M 2s
243350K .......... .......... .......... .......... .......... 91% 20.7M 2s
243400K .......... .......... .......... .......... .......... 91% 122M 2s
243450K .......... .......... .......... .......... .......... 91% 18.0M 2s
243500K .......... .......... .......... .......... .......... 91% 22.1M 2s
243550K .......... .......... .......... .......... .......... 91% 44.7M 2s
243600K .......... .......... .......... .......... .......... 91% 16.6M 2s
243650K .......... .......... .......... .......... .......... 91% 40.8M 2s
243700K .......... .......... .......... .......... .......... 91% 30.6M 2s
243750K .......... .......... .......... .......... .......... 91% 31.7M 2s
243800K .......... .......... .......... .......... .......... 91% 21.6M 2s
243850K .......... .......... .......... .......... .......... 91% 26.1M 2s
243900K .......... .......... .......... .......... .......... 91% 35.7M 2s
243950K .......... .......... .......... .......... .......... 91% 21.4M 2s
244000K .......... .......... .......... .......... .......... 91% 36.3M 2s
244050K .......... .......... .......... .......... .......... 91% 21.2M 2s
244100K .......... .......... .......... .......... .......... 91% 18.3M 2s
244150K .......... .......... .......... .......... .......... 91% 113M 2s
244200K .......... .......... .......... .......... .......... 91% 27.2M 2s
244250K .......... .......... .......... .......... .......... 91% 22.0M 2s
244300K .......... .......... .......... .......... .......... 91% 35.5M 2s
244350K .......... .......... .......... .......... .......... 91% 95.6M 2s
244400K .......... .......... .......... .......... .......... 91% 11.3M 2s
244450K .......... .......... .......... .......... .......... 92% 86.0M 2s
244500K .......... .......... .......... .......... .......... 92% 80.1M 2s
244550K .......... .......... .......... .......... .......... 92% 11.5M 2s
244600K .......... .......... .......... .......... .......... 92% 36.8M 2s
244650K .......... .......... .......... .......... .......... 92% 84.6M 2s
244700K .......... .......... .......... .......... .......... 92% 12.4M 2s
244750K .......... .......... .......... .......... .......... 92% 92.6M 2s
244800K .......... .......... .......... .......... .......... 92% 113M 2s
244850K .......... .......... .......... .......... .......... 92% 16.5M 2s
244900K .......... .......... .......... .......... .......... 92% 18.9M 2s
244950K .......... .......... .......... .......... .......... 92% 122M 2s
245000K .......... .......... .......... .......... .......... 92% 32.6M 2s
245050K .......... .......... .......... .......... .......... 92% 12.4M 2s
245100K .......... .......... .......... .......... .......... 92% 63.0M 2s
245150K .......... .......... .......... .......... .......... 92% 65.9M 2s
245200K .......... .......... .......... .......... .......... 92% 13.4M 2s
245250K .......... .......... .......... .......... .......... 92% 75.2M 2s
245300K .......... .......... .......... .......... .......... 92% 223M 2s
245350K .......... .......... .......... .......... .......... 92% 10.2M 2s
245400K .......... .......... .......... .......... .......... 92% 51.0M 2s
245450K .......... .......... .......... .......... .......... 92% 76.3M 2s
245500K .......... .......... .......... .......... .......... 92% 12.3M 2s
245550K .......... .......... .......... .......... .......... 92% 60.6M 2s
245600K .......... .......... .......... .......... .......... 92% 51.7M 2s
245650K .......... .......... .......... .......... .......... 92% 21.0M 2s
245700K .......... .......... .......... .......... .......... 92% 22.7M 2s
245750K .......... .......... .......... .......... .......... 92% 87.7M 2s
245800K .......... .......... .......... .......... .......... 92% 16.7M 2s
245850K .......... .......... .......... .......... .......... 92% 21.3M 2s
245900K .......... .......... .......... .......... .......... 92% 73.5M 2s
245950K .......... .......... .......... .......... .......... 92% 31.5M 2s
246000K .......... .......... .......... .......... .......... 92% 13.6M 2s
246050K .......... .......... .......... .......... .......... 92% 61.6M 2s
246100K .......... .......... .......... .......... .......... 92% 53.5M 2s
246150K .......... .......... .......... .......... .......... 92% 25.7M 2s
246200K .......... .......... .......... .......... .......... 92% 38.5M 2s
246250K .......... .......... .......... .......... .......... 92% 52.5M 2s
246300K .......... .......... .......... .......... .......... 92% 48.5M 2s
246350K .......... .......... .......... .......... .......... 92% 24.5M 2s
246400K .......... .......... .......... .......... .......... 92% 53.2M 2s
246450K .......... .......... .......... .......... .......... 92% 19.4M 2s
246500K .......... .......... .......... .......... .......... 92% 49.3M 2s
246550K .......... .......... .......... .......... .......... 92% 93.6M 2s
246600K .......... .......... .......... .......... .......... 92% 15.7M 2s
246650K .......... .......... .......... .......... .......... 92% 54.8M 2s
246700K .......... .......... .......... .......... .......... 92% 31.7M 2s
246750K .......... .......... .......... .......... .......... 92% 41.7M 2s
246800K .......... .......... .......... .......... .......... 92% 23.2M 2s
246850K .......... .......... .......... .......... .......... 92% 44.7M 1s
246900K .......... .......... .......... .......... .......... 92% 32.4M 1s
246950K .......... .......... .......... .......... .......... 92% 32.2M 1s
247000K .......... .......... .......... .......... .......... 92% 32.8M 1s
247050K .......... .......... .......... .......... .......... 92% 36.8M 1s
247100K .......... .......... .......... .......... .......... 93% 25.6M 1s
247150K .......... .......... .......... .......... .......... 93% 40.5M 1s
247200K .......... .......... .......... .......... .......... 93% 38.4M 1s
247250K .......... .......... .......... .......... .......... 93% 25.6M 1s
247300K .......... .......... .......... .......... .......... 93% 21.8M 1s
247350K .......... .......... .......... .......... .......... 93% 51.9M 1s
247400K .......... .......... .......... .......... .......... 93% 71.1M 1s
247450K .......... .......... .......... .......... .......... 93% 17.3M 1s
247500K .......... .......... .......... .......... .......... 93% 53.2M 1s
247550K .......... .......... .......... .......... .......... 93% 37.6M 1s
247600K .......... .......... .......... .......... .......... 93% 23.0M 1s
247650K .......... .......... .......... .......... .......... 93% 30.8M 1s
247700K .......... .......... .......... .......... .......... 93% 43.9M 1s
247750K .......... .......... .......... .......... .......... 93% 42.2M 1s
247800K .......... .......... .......... .......... .......... 93% 33.8M 1s
247850K .......... .......... .......... .......... .......... 93% 22.2M 1s
247900K .......... .......... .......... .......... .......... 93% 59.3M 1s
247950K .......... .......... .......... .......... .......... 93% 23.5M 1s
248000K .......... .......... .......... .......... .......... 93% 27.8M 1s
248050K .......... .......... .......... .......... .......... 93% 59.5M 1s
248100K .......... .......... .......... .......... .......... 93% 27.9M 1s
248150K .......... .......... .......... .......... .......... 93% 43.7M 1s
248200K .......... .......... .......... .......... .......... 93% 26.2M 1s
248250K .......... .......... .......... .......... .......... 93% 35.4M 1s
248300K .......... .......... .......... .......... .......... 93% 31.2M 1s
248350K .......... .......... .......... .......... .......... 93% 27.2M 1s
248400K .......... .......... .......... .......... .......... 93% 50.0M 1s
248450K .......... .......... .......... .......... .......... 93% 33.0M 1s
248500K .......... .......... .......... .......... .......... 93% 38.6M 1s
248550K .......... .......... .......... .......... .......... 93% 28.6M 1s
248600K .......... .......... .......... .......... .......... 93% 32.0M 1s
248650K .......... .......... .......... .......... .......... 93% 34.8M 1s
248700K .......... .......... .......... .......... .......... 93% 40.8M 1s
248750K .......... .......... .......... .......... .......... 93% 28.7M 1s
248800K .......... .......... .......... .......... .......... 93% 43.8M 1s
248850K .......... .......... .......... .......... .......... 93% 27.8M 1s
248900K .......... .......... .......... .......... .......... 93% 45.7M 1s
248950K .......... .......... .......... .......... .......... 93% 30.2M 1s
249000K .......... .......... .......... .......... .......... 93% 31.9M 1s
249050K .......... .......... .......... .......... .......... 93% 48.9M 1s
249100K .......... .......... .......... .......... .......... 93% 23.6M 1s
249150K .......... .......... .......... .......... .......... 93% 55.2M 1s
249200K .......... .......... .......... .......... .......... 93% 31.7M 1s
249250K .......... .......... .......... .......... .......... 93% 24.5M 1s
249300K .......... .......... .......... .......... .......... 93% 61.3M 1s
249350K .......... .......... .......... .......... .......... 93% 24.9M 1s
249400K .......... .......... .......... .......... .......... 93% 39.6M 1s
249450K .......... .......... .......... .......... .......... 93% 51.3M 1s
249500K .......... .......... .......... .......... .......... 93% 26.5M 1s
249550K .......... .......... .......... .......... .......... 93% 50.2M 1s
249600K .......... .......... .......... .......... .......... 93% 36.2M 1s
249650K .......... .......... .......... .......... .......... 93% 45.9M 1s
249700K .......... .......... .......... .......... .......... 93% 22.4M 1s
249750K .......... .......... .......... .......... .......... 94% 64.1M 1s
249800K .......... .......... .......... .......... .......... 94% 38.2M 1s
249850K .......... .......... .......... .......... .......... 94% 34.3M 1s
249900K .......... .......... .......... .......... .......... 94% 23.8M 1s
249950K .......... .......... .......... .......... .......... 94% 45.0M 1s
250000K .......... .......... .......... .......... .......... 94% 35.2M 1s
250050K .......... .......... .......... .......... .......... 94% 46.1M 1s
250100K .......... .......... .......... .......... .......... 94% 35.6M 1s
250150K .......... .......... .......... .......... .......... 94% 24.1M 1s
250200K .......... .......... .......... .......... .......... 94% 24.3M 1s
250250K .......... .......... .......... .......... .......... 94% 81.5M 1s
250300K .......... .......... .......... .......... .......... 94% 33.2M 1s
250350K .......... .......... .......... .......... .......... 94% 26.5M 1s
250400K .......... .......... .......... .......... .......... 94% 32.2M 1s
250450K .......... .......... .......... .......... .......... 94% 29.6M 1s
250500K .......... .......... .......... .......... .......... 94% 34.9M 1s
250550K .......... .......... .......... .......... .......... 94% 29.7M 1s
250600K .......... .......... .......... .......... .......... 94% 63.3M 1s
250650K .......... .......... .......... .......... .......... 94% 27.9M 1s
250700K .......... .......... .......... .......... .......... 94% 21.4M 1s
250750K .......... .......... .......... .......... .......... 94% 49.5M 1s
250800K .......... .......... .......... .......... .......... 94% 38.5M 1s
250850K .......... .......... .......... .......... .......... 94% 24.9M 1s
250900K .......... .......... .......... .......... .......... 94% 49.0M 1s
250950K .......... .......... .......... .......... .......... 94% 26.2M 1s
251000K .......... .......... .......... .......... .......... 94% 73.7M 1s
251050K .......... .......... .......... .......... .......... 94% 26.7M 1s
251100K .......... .......... .......... .......... .......... 94% 65.1M 1s
251150K .......... .......... .......... .......... .......... 94% 22.8M 1s
251200K .......... .......... .......... .......... .......... 94% 50.5M 1s
251250K .......... .......... .......... .......... .......... 94% 37.0M 1s
251300K .......... .......... .......... .......... .......... 94% 39.9M 1s
251350K .......... .......... .......... .......... .......... 94% 26.3M 1s
251400K .......... .......... .......... .......... .......... 94% 31.7M 1s
251450K .......... .......... .......... .......... .......... 94% 53.3M 1s
251500K .......... .......... .......... .......... .......... 94% 43.3M 1s
251550K .......... .......... .......... .......... .......... 94% 31.7M 1s
251600K .......... .......... .......... .......... .......... 94% 28.1M 1s
251650K .......... .......... .......... .......... .......... 94% 51.6M 1s
251700K .......... .......... .......... .......... .......... 94% 33.1M 1s
251750K .......... .......... .......... .......... .......... 94% 25.2M 1s
251800K .......... .......... .......... .......... .......... 94% 47.7M 1s
251850K .......... .......... .......... .......... .......... 94% 33.9M 1s
251900K .......... .......... .......... .......... .......... 94% 108M 1s
251950K .......... .......... .......... .......... .......... 94% 17.3M 1s
252000K .......... .......... .......... .......... .......... 94% 63.8M 1s
252050K .......... .......... .......... .......... .......... 94% 41.8M 1s
252100K .......... .......... .......... .......... .......... 94% 20.8M 1s
252150K .......... .......... .......... .......... .......... 94% 39.3M 1s
252200K .......... .......... .......... .......... .......... 94% 48.9M 1s
252250K .......... .......... .......... .......... .......... 94% 53.8M 1s
252300K .......... .......... .......... .......... .......... 94% 17.7M 1s
252350K .......... .......... .......... .......... .......... 94% 66.7M 1s
252400K .......... .......... .......... .......... .......... 94% 71.3M 1s
252450K .......... .......... .......... .......... .......... 95% 43.7M 1s
252500K .......... .......... .......... .......... .......... 95% 17.0M 1s
252550K .......... .......... .......... .......... .......... 95% 109M 1s
252600K .......... .......... .......... .......... .......... 95% 46.3M 1s
252650K .......... .......... .......... .......... .......... 95% 52.3M 1s
252700K .......... .......... .......... .......... .......... 95% 16.1M 1s
252750K .......... .......... .......... .......... .......... 95% 100M 1s
252800K .......... .......... .......... .......... .......... 95% 35.2M 1s
252850K .......... .......... .......... .......... .......... 95% 50.8M 1s
252900K .......... .......... .......... .......... .......... 95% 20.3M 1s
252950K .......... .......... .......... .......... .......... 95% 76.6M 1s
253000K .......... .......... .......... .......... .......... 95% 29.6M 1s
253050K .......... .......... .......... .......... .......... 95% 20.5M 1s
253100K .......... .......... .......... .......... .......... 95% 64.4M 1s
253150K .......... .......... .......... .......... .......... 95% 94.5M 1s
253200K .......... .......... .......... .......... .......... 95% 30.8M 1s
253250K .......... .......... .......... .......... .......... 95% 21.6M 1s
253300K .......... .......... .......... .......... .......... 95% 7.70M 1s
253350K .......... .......... .......... .......... .......... 95% 102M 1s
253400K .......... .......... .......... .......... .......... 95% 107M 1s
253450K .......... .......... .......... .......... .......... 95% 78.1M 1s
253500K .......... .......... .......... .......... .......... 95% 104M 1s
253550K .......... .......... .......... .......... .......... 95% 79.7M 1s
253600K .......... .......... .......... .......... .......... 95% 40.1M 1s
253650K .......... .......... .......... .......... .......... 95% 36.8M 1s
253700K .......... .......... .......... .......... .......... 95% 33.3M 1s
253750K .......... .......... .......... .......... .......... 95% 18.9M 1s
253800K .......... .......... .......... .......... .......... 95% 123M 1s
253850K .......... .......... .......... .......... .......... 95% 16.2M 1s
253900K .......... .......... .......... .......... .......... 95% 47.9M 1s
253950K .......... .......... .......... .......... .......... 95% 22.7M 1s
254000K .......... .......... .......... .......... .......... 95% 34.4M 1s
254050K .......... .......... .......... .......... .......... 95% 60.3M 1s
254100K .......... .......... .......... .......... .......... 95% 23.5M 1s
254150K .......... .......... .......... .......... .......... 95% 25.6M 1s
254200K .......... .......... .......... .......... .......... 95% 28.1M 1s
254250K .......... .......... .......... .......... .......... 95% 96.4M 1s
254300K .......... .......... .......... .......... .......... 95% 20.9M 1s
254350K .......... .......... .......... .......... .......... 95% 29.3M 1s
254400K .......... .......... .......... .......... .......... 95% 25.5M 1s
254450K .......... .......... .......... .......... .......... 95% 19.3M 1s
254500K .......... .......... .......... .......... .......... 95% 174M 1s
254550K .......... .......... .......... .......... .......... 95% 27.4M 1s
254600K .......... .......... .......... .......... .......... 95% 29.7M 1s
254650K .......... .......... .......... .......... .......... 95% 39.9M 1s
254700K .......... .......... .......... .......... .......... 95% 18.7M 1s
254750K .......... .......... .......... .......... .......... 95% 109M 1s
254800K .......... .......... .......... .......... .......... 95% 35.4M 1s
254850K .......... .......... .......... .......... .......... 95% 17.0M 1s
254900K .......... .......... .......... .......... .......... 95% 30.3M 1s
254950K .......... .......... .......... .......... .......... 95% 17.8M 1s
255000K .......... .......... .......... .......... .......... 95% 105M 1s
255050K .......... .......... .......... .......... .......... 95% 28.3M 1s
255100K .......... .......... .......... .......... .......... 96% 24.5M 1s
255150K .......... .......... .......... .......... .......... 96% 16.6M 1s
255200K .......... .......... .......... .......... .......... 96% 116M 1s
255250K .......... .......... .......... .......... .......... 96% 25.4M 1s
255300K .......... .......... .......... .......... .......... 96% 28.5M 1s
255350K .......... .......... .......... .......... .......... 96% 50.5M 1s
255400K .......... .......... .......... .......... .......... 96% 17.6M 1s
255450K .......... .......... .......... .......... .......... 96% 63.1M 1s
255500K .......... .......... .......... .......... .......... 96% 25.8M 1s
255550K .......... .......... .......... .......... .......... 96% 21.3M 1s
255600K .......... .......... .......... .......... .......... 96% 37.7M 1s
255650K .......... .......... .......... .......... .......... 96% 16.7M 1s
255700K .......... .......... .......... .......... .......... 96% 124M 1s
255750K .......... .......... .......... .......... .......... 96% 25.6M 1s
255800K .......... .......... .......... .......... .......... 96% 23.8M 1s
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2024-05-30 12:19:12 (12.9 MB/s) - ‘ESPbeta.tgz’ saved [272121672/272121672]
+ tar -xf ESPbeta.tgz
+ rm -rf EngSketchPad/data/Slugs
+ python --version
Python 3.11.9
+ [[ '' == *\.\i\f\o\r\t ]]
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/config/
+ ./makeEnv
ESP runtime AutoConfigurator
CASROOT = /home/jenkins/util/ESP/OpenCASCADE-7.7.0 with contents:
bin
include
lib
share
Info: Python exec /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/python found!
Info: Python header /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11/Python.h found!
Info: Python library /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/libpython3.11.so found!
ESP_ARCH = LINUX64
ESP_ROOT = /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad
EFCOMP = gfortran
CARCH = LINUX64
CASROOT = /home/jenkins/util/ESP/OpenCASCADE-7.7.0
CASARCH = .
CASREV = 7.7
PYTHONINC= /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11
PYTHONLIB= -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
+ source /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=LINUX64
++ ESP_ARCH=LINUX64
++ export ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad
++ ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad
++ export CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.7.0
++ CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.7.0
++ export CASARCH=.
++ CASARCH=.
++ export CASREV=7.7
++ CASREV=7.7
++ export PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/home/jenkins/.local/bin:/home/jenkins/bin:/usr/local/bin:/usr/bin:/usr/local/sbin:/usr/sbin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONINC=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11
++ PYTHONINC=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11
++ export 'PYTHONLIB=-L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11'
++ PYTHONLIB='-L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11'
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ export AFLR_ARCH=Linux-x86-64
++ AFLR_ARCH=Linux-x86-64
++ '[' -z /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib: ']'
++ export LD_LIBRARY_PATH=/home/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ LD_LIBRARY_PATH=/home/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ export UDUNITS2_XML_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ export CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ export TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ export 'SLUGS_START=firefox /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/SLUGS/Slugs.html &'
++ SLUGS_START='firefox /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/SLUGS/Slugs.html &'
++ export 'ESP_START=firefox /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/ESP/ESP.html &'
++ ESP_START='firefox /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/ESP/ESP.html &'
++ export 'WV_START=firefox /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/wvClient/wv.html &'
++ WV_START='firefox /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/wvClient/wv.html &'
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src
+ make
(cd EGADS/src; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/src'
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/LINUX64
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/LINUX64
cp -p ../include/LINUX64 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/LINUX64
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/STANALYZER.make
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/STANALYZER.make
cp -p ../include/STANALYZER.make /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/STANALYZER.make
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads.h
cp -p ../include/egads.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads_dot.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads_dot.h
cp -p ../include/egads_dot.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads_dot.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads.inc
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads.inc
cp -p ../include/egads.inc /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads.inc
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsErrors.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsErrors.h
cp -p ../include/egadsErrors.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsErrors.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsTypes.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsTypes.h
cp -p ../include/egadsTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsTypes.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/emp.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/emp.h
cp -p ../include/emp.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/emp.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/prm.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/prm.h
cp -p ../include/prm.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/prm.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsserver.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsserver.h
cp -p ../include/wsserver.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsserver.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsserver.inc
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsserver.inc
cp -p ../include/wsserver.inc /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsserver.inc
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsss.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsss.h
cp -p ../include/wsss.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsss.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsTris.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsTris.h
cp -p egadsTris.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsTris.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsSplineFit.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsSplineFit.h
cp -p egadsSplineFit.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsSplineFit.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsSplineVels.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsSplineVels.h
cp -p egadsSplineVels.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsSplineVels.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsf90.inc
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsf90.inc
cp -p ../include/egadsf90.inc /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsf90.inc
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal/SurrealD.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Lazy.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal/SurrealD_Lazy.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Trad.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal/SurrealD_Trad.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal/SurrealS.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Lazy.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal/SurrealS_Lazy.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Trad.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal/SurrealS_Trad.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/always_inline.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal/always_inline.h
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -I../include \
-I. egadsGeom.cpp -o ./egadsGeom.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -I../include \
-I. egadsHLevel.cpp -o ./egadsHLevel.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -I../include \
-I. egadsTopo.cpp -o ./egadsTopo.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -I../include \
-I. egadsCopy.cpp -o ./egadsCopy.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -I../include \
-I. egadsSpline.cpp -o ./egadsSpline.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -I../include \
-I. egadsIO.cpp -o ./egadsIO.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -I../include \
-I. egadsSplineFit.cpp -o ./egadsSplineFit.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -I../include \
-I. egadsSkinning.cpp -o ./egadsSkinning.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -I../include \
-I. egadsTessSens.cpp -o ./egadsTessSens.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include OCC/BRepLib_FuseEdges.cpp -o ./BRepLib_FuseEdges.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsBase.c -o ./egadsBase.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsMemory.c -o ./egadsMemory.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsAttrs.c -o ./egadsAttrs.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsTess.c -o ./egadsTess.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsTessInp.c -o ./egadsTessInp.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsTris.c -o ./egadsTris.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsQuads.c -o ./egadsQuads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsFit.c -o ./egadsFit.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsRobust.c -o ./egadsRobust.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsSBO.c -o ./egadsSBO.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap prmCfit.c -o ./prmCfit.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap prmGrid.c -o ./prmGrid.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap prmUV.c -o ./prmUV.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsExport.c -o ./egadsExport.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsEffect.c -o ./egadsEffect.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsSolids.c -o ./egadsSolids.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include ../util/emp.c \
-o ./emp.o
g++ -g -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -I. -I../include \
../util/evaluate.c -o ./evaluate.o
g++ -g -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.7 -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -I. -I../include \
../util/rational.c -o ./rational.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -I../include -I../util \
../util/regQuads.c -o ./regQuads.o
g++ -g -o ./SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp
./SurrealD1
SurrealD1_test_suite Complete!
g++ -g -o ./SurrealD4 -O -std=c++11 -I. ../util/SurrealD4_btest.cpp
./SurrealD4
SurrealD4_test_suite Complete!
g++ -g -o ./SurrealS1 -O -std=c++11 -I. ../util/SurrealS1_btest.cpp
./SurrealS1
SurrealS1_test_suite Complete!
g++ -g -o ./SurrealS4 -O -std=c++11 -I. ../util/SurrealS4_btest.cpp
../util/SurrealS4_btest.cpp: In function ‘void multiply_deriv2()’:
../util/SurrealS4_btest.cpp:1265:23: note: variable tracking size limit exceeded with -fvar-tracking-assignments, retrying without
BOOST_AUTO_TEST_CASE( multiply_deriv2 )
^~~~~~~~~~~~~~~
../util/SurrealS4_btest.cpp:19:42: note: in definition of macro ‘BOOST_AUTO_TEST_CASE’
#define BOOST_AUTO_TEST_CASE( fun ) void fun()
^~~
./SurrealS4
SurrealS4_test_suite Complete!
make -C ../util
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/util'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 uvmap/main/uvmap.c -Iuvmap \
-o ./uvmap.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_bnd_adj.c -o ./uvmap_bnd_adj.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_ibfibf.c -o ./uvmap_ibfibf.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_message.c -o ./uvmap_message.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_ibfin.c -o ./uvmap_ibfin.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_read.c -o ./uvmap_read.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_iccin.c -o ./uvmap_iccin.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_add.c -o ./uvmap_add.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_cpu_message.c -o ./uvmap_cpu_message.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/EG_uvmapFindUV.c -o ./EG_uvmapFindUV.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/EG_uvmapTest.c -o ./EG_uvmapTest.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_inibe.c -o ./uvmap_inibe.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_version.c -o ./uvmap_version.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_inl_uv_bnd.c -o ./uvmap_inl_uv_bnd.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_chk_edge_ratio.c -o ./uvmap_chk_edge_ratio.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_struct_tasks.c -o ./uvmap_struct_tasks.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/EG_uvmap_Read.c -o ./EG_uvmap_Read.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_idibe.c -o ./uvmap_idibe.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/EG_uvmapStructFree.c -o ./EG_uvmapStructFree.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/EG_uvmapGen.c -o ./EG_uvmapGen.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_write.c -o ./uvmap_write.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_ibeibe.c -o ./uvmap_ibeibe.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_chk_area_uv.c -o ./uvmap_chk_area_uv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_norm_uv.c -o ./uvmap_norm_uv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_iccibe.c -o ./uvmap_iccibe.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_malloc.c -o ./uvmap_malloc.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_gen_uv.c -o ./uvmap_gen_uv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_to_egads.c -o ./uvmap_to_egads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/EG_uvmap_Write.c -o ./EG_uvmap_Write.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_test.c -o ./uvmap_test.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_mben_disc.c -o ./uvmap_mben_disc.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_find_uv.c -o ./uvmap_find_uv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_gen.c -o ./uvmap_gen.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_solve.c -o ./uvmap_solve.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. uvmap/uvmap_from_egads.c -o ./uvmap_from_egads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 egadsUVmap.c -Iuvmap \
-o ./egadsUVmap.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libuvmap.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libuvmap.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libuvmap.a ./egadsUVmap.o uvmap_cpu_message.o uvmap_ibfibf.o uvmap_message.o uvmap_version.o uvmap_gen_uv.o uvmap_inl_uv_bnd.o EG_uvmap_Read.o uvmap_chk_edge_ratio.o uvmap_idibe.o uvmap_write.o uvmap_ibeibe.o uvmap_chk_area_uv.o uvmap_gen.o uvmap_malloc.o uvmap_to_egads.o EG_uvmap_Write.o uvmap_iccibe.o EG_uvmapGen.o EG_uvmapTest.o uvmap_read.o uvmap_ibfin.o uvmap_iccin.o uvmap_add.o EG_uvmapFindUV.o uvmap_struct_tasks.o uvmap_bnd_adj.o EG_uvmapStructFree.o uvmap_inibe.o uvmap_norm_uv.o uvmap_test.o uvmap_mben_disc.o uvmap_find_uv.o uvmap_solve.o uvmap_from_egads.o; )
ar: creating /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libuvmap.a
gcc -g -o ./uvmap.exe ./uvmap.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -luvmap -lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/util'
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegads.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegads.so
(cd .; gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegads.so \
egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o emp.o evaluate.o rational.o regQuads.o \
-L/home/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet -pthread -lm -lstdc++ -lrt )
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadstatic.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadstatic.a
cp /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libuvmap.a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadstatic.a
(cd .; \
ar rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadstatic.a egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o emp.o \
evaluate.o rational.o regQuads.o; )
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include fgadsBase.c -o ./fgadsBase.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include fgadsMemory.c -o ./fgadsMemory.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include fgadsAttrs.c -o ./fgadsAttrs.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include fgadsTess.c -o ./fgadsTess.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include fgadsHLevel.c -o ./fgadsHLevel.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include fgadsGeom.c -o ./fgadsGeom.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include fgadsTopo.c -o ./fgadsTopo.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libfgads.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libfgads.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libfgads.a fgadsBase.o fgadsMemory.o fgadsAttrs.o fgadsTess.o fgadsHLevel.o fgadsGeom.o fgadsTopo.o; )
ar: creating /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libfgads.a
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libemp.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libemp.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libemp.a emp.o; )
ar: creating /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libemp.a
*** EGADS Build Complete! ***
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/src'
(cd EGADS/lite; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/lite'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteBase.c -o ./liteBase.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteMemory.c -o ./liteMemory.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteGeom.c -o ./liteGeom.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteTopo.c -o ./liteTopo.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteAttrs.c -o ./liteAttrs.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteImport.c -o ./liteImport.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteString.c -o ./liteString.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -DLITE -I../include -I. -I../src \
../src/egadsTess.c -o ./liteTess.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -DLITE -I../include -I. -I../src \
../src/egadsTris.c -o ./liteTris.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I. -I../src \
../src/egadsQuads.c -o ./liteQuads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -DLITE -I../include -I. -I../src \
-I../util ../src/egadsTessInp.c -o ./liteTessInp.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 ../src/egadsRobust.c \
-o ./egadsRobust.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -DLINUX64 -I../include ../util/emp.c \
-o ./emp.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -DLITE -I../include -I. -I../src \
../util/evaluate.c -o ./evaLite.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -DLITE ../util/rational.c \
-o ./ratLite.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -DLITE -I../include -I../util \
../util/regQuads.c -o ./liteRegQuads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -DLITE -I../include -I. -I../src \
../src/egadsEffect.c -o ./liteEffect.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -DLITE -I../include -I. -I../src \
-I../util/uvmap liteUVmap.c -o ./liteUVmap.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadslite.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadslite.so
(cd .; gcc -g -shared -Wl,-no-undefined \
-o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadslite.so liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o liteTess.o liteTris.o \
liteQuads.o liteTessInp.o egadsRobust.o emp.o evaLite.o \
ratLite.o liteRegQuads.o liteEffect.o liteUVmap.o \
-lpthread -lm )
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadslitestatic.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadslitestatic.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadslitestatic.a liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o \
liteTess.o liteTris.o liteQuads.o liteTessInp.o egadsRobust.o \
emp.o evaLite.o ratLite.o liteRegQuads.o liteEffect.o \
liteUVmap.o ; )
ar: creating /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadslitestatic.a
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/lite'
(cd wvServer; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/wvServer'
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 map.cpp -o ./map.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include base64-decode.c -o ./base64-decode.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include handshake.c -o ./handshake.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include client-handshake.c -o ./client-handshake.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include libwebsockets.c -o ./libwebsockets.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include extension-deflate-stream.c -o ./extension-deflate-stream.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include md5.c -o ./md5.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include extension-x-google-mux.c -o ./extension-x-google-mux.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include parsers.c -o ./parsers.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include extension.c -o ./extension.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include sha-1.c -o ./sha-1.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include server.c -o ./server.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include wv.c -o ./wv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include browserMessage.c -o ./browserMessage.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include fwv.c -o ./fwv.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libwsserver.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libwsserver.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libwsserver.a map.o base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o \
./fwv.o; )
ar: creating /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libwsserver.a
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -DSTANDALONE server.c \
-I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. -o ./servertest.o
g++ -g -o ./server ./servertest.o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libwsserver.a \
-lpthread -lz -lm
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libwsserver.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libwsserver.so
(cd .; g++ -g -shared -Wl,-no-undefined \
-o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libwsserver.so base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o map.o -lz -lpthread)
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/wvServer'
(cd EGADS/examples; make -f egads2cart.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/examples'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include egads2cart.c \
-o ./egads2cart.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/egads2cart ./egads2cart.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -legads \
-lrt -lm
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vCurvature.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/examples'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include vCurvature.c -o ./vCurvature.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/vCurvature ./vCurvature.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lwsserver -legads -lrt
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vGeom.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/examples'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include vGeom.c -o ./vGeom.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/vGeom ./vGeom.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lwsserver -legads \
-lrt
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vTess.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/examples'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include vTess.c -o ./vTess.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include ../util/retessFaces.c \
-o ./retessFaces.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/vTesstatic ./vTess.o ./retessFaces.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lwsserver -legadstatic -L/home/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet -pthread -lm \
-lpthread -lz -lrt -lm
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/vTess ./vTess.o ./retessFaces.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lwsserver -legads -lrt
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/examples'
(cd OpenCSM; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/OpenCSM'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. serveCSM.c -o ./serveCSM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. OpenCSM.c -o ./OpenCSM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udp.c -o ./udp.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. tim.c -o ./tim.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libocsm.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libocsm.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libocsm.so ./OpenCSM.o ./udp.o ./tim.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -legads -lwsserver -ldl -lrt -lm
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/serveCSM ./serveCSM.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. serveESP.c -o ./serveESP.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/serveESP ./serveESP.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. sensCSM.c -o ./sensCSM.o
gcc -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/sensCSM ./sensCSM.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lrt -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpBezier.c -o ./udpBezier.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bezier.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bezier.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bezier.so ./udpBezier.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpBiconvex.c -o ./udpBiconvex.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/biconvex.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/biconvex.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/biconvex.so ./udpBiconvex.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpBox.c -o ./udpBox.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/box.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/box.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/box.so ./udpBox.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpBspline.c -o ./udpBspline.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bspline.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bspline.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bspline.so ./udpBspline.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfCatmull.c -o ./udfCatmull.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/catmull.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/catmull.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/catmull.so ./udfCatmull.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfCompare.c -o ./udfCompare.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/compare.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/compare.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/compare.so ./udfCompare.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfCreateBEM.c -o ./udfCreateBEM.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/createBEM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/createBEM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/createBEM.so ./udfCreateBEM.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfCreatePoly.c -o ./udfCreatePoly.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/createPoly.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/createPoly.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/createPoly.so ./udfCreatePoly.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpCsm.c -o ./udpCsm.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/csm.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/csm.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/csm.so ./udpCsm.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfDeform.c -o ./udfDeform.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/deform.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/deform.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/deform.so ./udfDeform.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfDroop.c -o ./udfDroop.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/droop.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/droop.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/droop.so ./udfDroop.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfDumpPmtrs.c -o ./udfDumpPmtrs.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/dumpPmtrs.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/dumpPmtrs.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/dumpPmtrs.so ./udfDumpPmtrs.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfEditAttr.c -o ./udfEditAttr.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/editAttr.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/editAttr.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/editAttr.so ./udfEditAttr.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpEllipse.c -o ./udpEllipse.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ellipse.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ellipse.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ellipse.so ./udpEllipse.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpEqn2body.c -o ./udpEqn2body.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/eqn2body.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/eqn2body.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/eqn2body.so ./udpEqn2body.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpFitcurve.c -o ./udpFitcurve.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/fitcurve.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/fitcurve.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/fitcurve.so ./udpFitcurve.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfFlend.c -o ./udfFlend.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/flend.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/flend.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/flend.so ./udfFlend.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpFreeform.c -o ./udpFreeform.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/freeform.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/freeform.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/freeform.so ./udpFreeform.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfGanged.c -o ./udfGanged.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ganged.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ganged.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ganged.so ./udfGanged.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfGuide.c -o ./udfGuide.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/guide.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/guide.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/guide.so ./udfGuide.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpHex.c -o ./udpHex.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/hex.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/hex.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/hex.so ./udpHex.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpImport.c -o ./udpImport.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/import.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/import.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/import.so ./udpImport.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpKulfan.c -o ./udpKulfan.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/kulfan.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/kulfan.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/kulfan.so ./udpKulfan.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfLinalg.c -o ./udfLinalg.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/linalg.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/linalg.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/linalg.so ./udfLinalg.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfMatchBodys.c -o ./udfMatchBodys.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/matchBodys.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/matchBodys.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/matchBodys.so ./udfMatchBodys.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfMechanism.c -o ./udfMechanism.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mechanism.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mechanism.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mechanism.so ./udfMechanism.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpNaca.c -o ./udpNaca.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca.so ./udpNaca.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfNaca6mc.c -o ./udfNaca6mc.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca6mc.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca6mc.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca6mc.so ./udfNaca6mc.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfNacelle.c -o ./udfNacelle.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nacelle.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nacelle.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nacelle.so ./udfNacelle.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpNurbbody.c -o ./udpNurbbody.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nurbbody.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nurbbody.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nurbbody.so ./udpNurbbody.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfNuscale.c -o ./udfNuscale.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nuscale.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nuscale.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nuscale.so ./udfNuscale.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfOffset.c -o ./udfOffset.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/offset.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/offset.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/offset.so ./udfOffset.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpParabaloid.c -o ./udpParabaloid.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/parabaloid.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/parabaloid.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/parabaloid.so ./udpParabaloid.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpParsec.cpp -o ./udpParsec.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/parsec.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/parsec.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/parsec.so ./udpParsec.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpPod.c -o ./udpPod.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pod.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pod.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pod.so ./udpPod.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpPoly.c -o ./udpPoly.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/poly.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/poly.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/poly.so ./udpPoly.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfPrintBbox.c -o ./udfPrintBbox.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printBbox.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printBbox.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printBbox.so ./udfPrintBbox.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfPrintBrep.c -o ./udfPrintBrep.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printBrep.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printBrep.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printBrep.so ./udfPrintBrep.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfPrintEgo.c -o ./udfPrintEgo.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printEgo.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printEgo.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printEgo.so ./udfPrintEgo.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpProp.c -o ./udpProp.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/prop.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/prop.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/prop.so ./udpProp.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpRadwaf.c -o ./udpRadwaf.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/radwaf.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/radwaf.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/radwaf.so ./udpRadwaf.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpSample.c -o ./udpSample.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/sample.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/sample.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/sample.so ./udpSample.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpSew.c -o ./udpSew.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/sew.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/sew.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/sew.so ./udpSew.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfShadow.c -o ./udfShadow.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/shadow.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/shadow.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/shadow.so ./udfShadow.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfSlices.c -o ./udfSlices.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/slices.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/slices.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/slices.so ./udfSlices.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpStag.c -o ./udpStag.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stag.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stag.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stag.so ./udpStag.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfStiffener.c -o ./udfStiffener.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stiffener.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stiffener.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stiffener.so ./udfStiffener.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpSupell.c -o ./udpSupell.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/supell.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/supell.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/supell.so ./udpSupell.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfTester1.c -o ./udfTester1.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tester1.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tester1.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tester1.so ./udfTester1.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpTester2.c -o ./udpTester2.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tester2.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tester2.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tester2.so ./udpTester2.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpVsp3.c -o ./udpVsp3.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vsp3.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vsp3.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vsp3.so ./udpVsp3.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpWaffle.c -o ./udpWaffle.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/waffle.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/waffle.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/waffle.so ./udpWaffle.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpWarp.c -o ./udpWarp.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/warp.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/warp.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/warp.so ./udpWarp.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. eggPDT2.c -o ./eggPDT2.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/PDT2.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/PDT2.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/PDT2.so ./eggPDT2.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpNaca456.c -o ./udpNaca456.o
gfortran -g -c -O -fPIC -frecursive -fcray-pointer naca456.f90 -o ./naca456.o -J .
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca456.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca456.so
gfortran -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca456.so ./udpNaca456.o ./naca456.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timEreped.c -o ./timEreped.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ereped.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ereped.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ereped.so ./timEreped.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timMitten.c -o ./timMitten.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mitten.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mitten.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mitten.so ./timMitten.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timPlotter.c -o ./timPlotter.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/plotter.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/plotter.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/plotter.so ./timPlotter.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timPlugs.c -o ./timPlugs.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/plugs.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/plugs.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/plugs.so ./timPlugs.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timSlugs.c -o ./timSlugs.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/slugs.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/slugs.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/slugs.so ./timSlugs.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timVspSetup.c -o ./timVspSetup.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vspSetup.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vspSetup.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vspSetup.so ./timVspSetup.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/OpenCSM.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/OpenCSM.h
cp -p OpenCSM.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/OpenCSM.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/common.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/common.h
cp -p common.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/common.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udp.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udp.h
cp -p udp.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udp.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/esp.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/esp.h
cp -p esp.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/esp.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/tim.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/tim.h
cp -p tim.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/tim.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egg.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egg.h
cp -p egg.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egg.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udpUtilities.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udpUtilities.h
cp -p udpUtilities.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udpUtilities.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udpUtilities.c
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udpUtilities.c
cp -p udpUtilities.c /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udpUtilities.c
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/OpenCSM'
(cd Slugs; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/Slugs'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. Slugs.c -o ./Slugs.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. Fitter.c \
-o ./Fitter.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. RedBlackTree.c \
-o ./RedBlackTree.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. Tessellate.c \
-o ./Tessellate.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/Slugs ./Slugs.o ./Fitter.o ./RedBlackTree.o \
./Tessellate.o -lrt -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lwsserver -legads \
-lpthread -lz -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. TestFit.c -o ./TestFit.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/TestFit ./TestFit.o ./Fitter.o -lrt -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -legads \
-lpthread -lz -lm
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/Slugs'
(cd CAPS; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS'
/bin/cp Cart3D/X86_64_GCC/libc3dio.a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libc3dio.a
/bin/cp Cart3D/X86_64_GCC/libCart3D.a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libCart3D.a
/bin/cp Executables/LINUX64/avl /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/avl
/bin/cp Executables/LINUX64/pplot /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/pplot
/bin/cp Executables/LINUX64/pxplot /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/pxplot
/bin/cp Executables/LINUX64/xfoil /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/xfoil
/bin/cp Executables/LINUX64/mastros.exe /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/mastros.exe
/bin/cp Executables/LINUX64/ASTRO.D01 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/ASTRO.D01
/bin/cp Executables/LINUX64/ASTRO.IDX /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/ASTRO.IDX
/bin/cp Executables/LINUX64/mses /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/mses
/bin/cp Executables/LINUX64/mset /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/mset
/bin/cp udunits/include/*.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include
/bin/cp udunits/LINUX64/libudunits2.so /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib
ln -sf libudunits2.so /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libudunits2.so.0
/bin/cp Libraries/LINUX64/aflr2AIM.so /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/aflr2AIM.so
/bin/cp Libraries/LINUX64/aflr3AIM.so /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/aflr3AIM.so
/bin/cp Libraries/LINUX64/aflr4AIM.so /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/aflr4AIM.so
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS'
(cd CAPS/src; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/src'
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/caps.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/caps.h
cp -p ../include/caps.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/caps.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/capsErrors.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/capsErrors.h
cp -p ../include/capsErrors.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/capsErrors.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/capsTypes.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/capsTypes.h
cp -p ../include/capsTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/capsTypes.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aimUtil.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aimUtil.h
cp -p ../include/aimUtil.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aimUtil.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aimMesh.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aimMesh.h
cp -p ../include/aimMesh.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aimMesh.h
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../include \
-I/usr/include/udunits2 aimUtil.c -o ./aimUtil.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include \
-I/usr/include/udunits2 aimTransferUtil.c \
-o ./aimTransferUtil.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../include \
aimMesh.c -o ./aimMesh.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libaimUtil.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libaimUtil.a
ar -rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libaimUtil.a ./aimUtil.o ./aimMesh.o \
./aimTransferUtil.o
ar: creating /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libaimUtil.a
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsBase.c -o ./capsBase.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsAnalysis.c -o ./capsAnalysis.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsApprox.c -o ./capsApprox.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsAttr.c -o ./capsAttr.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsAIM.c -o ./capsAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsBound.c -o ./capsBound.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsProblem.c -o ./capsProblem.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsValue.c -o ./capsValue.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsUnits.c -o ./capsUnits.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 conjGrad.c -o ./conjGrad.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsFunIDs.c -o ./capsFunIDs.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsChkInpt.c -o ./capsChkInpt.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 printObject.c -o ./printObject.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libcaps.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libcaps.so
(cd .; gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libcaps.so \
capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -ludunits2 -locsm -legads -ldl \
-lrt -lm )
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libcapsstatic.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libcapsstatic.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libcapsstatic.a capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o )
ar: creating /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libcapsstatic.a
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include testingAIM.c \
-o ./testingAIM.o
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingAIM.so
rm: cannot remove '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingAIM.so': No such file or directory
make[1]: [Makefile:23: /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingAIM.so] Error 1 (ignored)
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingAIM.so ./testingAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include testingWriter.c \
-o ./testingWriter.o
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingWriter.so
rm: cannot remove '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingWriter.so': No such file or directory
make[1]: [Makefile:33: /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingWriter.so] Error 1 (ignored)
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingWriter.so ./testingWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -ldl -lrt -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include phaseUtil.c \
-o ./phaseUtil.o
gcc -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/phaseUtil ./phaseUtil.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -ludunits2 -locsm -legads -ldl -lrt -lm
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/src'
(cd ../CAPSexamples; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples'
(make -C cCAPS -f aeroelastic_SU2.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o
gcc -g -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include avlTest.c -o ./avlTest.o
gcc -g -o ./avlTest ./avlTest.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include awaveTest.c -o ./awaveTest.o
gcc -g -o ./awaveTest ./awaveTest.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include frictionTest.c -o ./frictionTest.o
gcc -g -o ./frictionTest ./frictionTest.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include fun3dAFLR2Test.c -o ./fun3dAFLR2Test.o
gcc -g -o ./fun3dAFLR2Test ./fun3dAFLR2Test.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include fun3dTetgenTest.c -o ./fun3dTetgenTest.o
gcc -g -o ./fun3dTetgenTest ./fun3dTetgenTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include aeroelasticTest.c -o ./aeroelasticTest.o
gcc -g -o ./aeroelasticTest ./aeroelasticTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f hsm.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include hsmTest.c -o ./hsmTest.o
gcc -g -o ./hsmTest ./hsmTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include hsmSimplePlateTest.c -o ./hsmSimplePlateTest.o
gcc -g -o ./hsmSimplePlateTest ./hsmSimplePlateTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include hsmCantileverPlateTest.c -o ./hsmCantileverPlateTest.o
gcc -g -o ./hsmCantileverPlateTest ./hsmCantileverPlateTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include hsmJoinedPlateTest.c -o ./hsmJoinedPlateTest.o
gcc -g -o ./hsmJoinedPlateTest ./hsmJoinedPlateTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include interferenceTest.c \
-o ./interferenceTest.o
gcc -g -o ./interferenceTest ./interferenceTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include msesTest.c -o ./msesTest.o
gcc -g -o ./msesTest ./msesTest.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f mystran.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include mystranTest.c -o ./mystranTest.o
gcc -g -o ./mystranTest ./mystranTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include pointwiseTest.c -o ./pointwiseTest.o
gcc -g -o ./pointwiseTest ./pointwiseTest.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples'
(cd CAPS/aim; make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim'
make -C utils
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/utils'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython attrUtils.c -o ./attrUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython meshUtils.c -o ./meshUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cfdUtils.c -o ./cfdUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython miscUtils.c -o ./miscUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython feaUtils.c -o ./feaUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython vlmUtils.c -o ./vlmUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranUtils.c -o ./nastranUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython tecplotUtils.c -o ./tecplotUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython arrayUtils.c -o ./arrayUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython deprecateUtils.c -o ./deprecateUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cardUtils.c -o ./cardUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranCards.c -o ./nastranCards.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython jsonUtils.c -o ./jsonUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cython/nastranOP2Reader.c -o ./nastranOP2Reader.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. vlmSpanSpace.cpp -o ./vlmSpanSpace.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libutils.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libutils.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libutils.a attrUtils.o meshUtils.o cfdUtils.o miscUtils.o feaUtils.o vlmUtils.o nastranUtils.o tecplotUtils.o arrayUtils.o deprecateUtils.o cardUtils.o nastranCards.o jsonUtils.o nastranOP2Reader.o vlmSpanSpace.o )
ar: creating /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libutils.a
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils
cp -p -f attrUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/attrUtils.h
cp -p -f nastranCards.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/nastranCards.h
cp -p -f cfdTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/cfdTypes.h
cp -p -f arrayUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/arrayUtils.h
cp -p -f meshUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/meshUtils.h
cp -p -f feaTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/feaTypes.h
cp -p -f miscUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/miscUtils.h
cp -p -f meshTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/meshTypes.h
cp -p -f attrTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/attrTypes.h
cp -p -f vlmTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/vlmTypes.h
cp -p -f feaUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/feaUtils.h
cp -p -f cfdUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/cfdUtils.h
cp -p -f vlmUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/vlmUtils.h
cp -p -f cardTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/cardTypes.h
cp -p -f jsonUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/jsonUtils.h
cp -p -f nastranUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/nastranUtils.h
cp -p -f deprecateUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/deprecateUtils.h
cp -p -f miscTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/miscTypes.h
cp -p -f tecplotUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/tecplotUtils.h
cp -p -f vlmSpanSpace.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/vlmSpanSpace.h
cp -p -f cardUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/cardUtils.h
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/utils'
make -C friction
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/friction'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -Wno-format -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils frictionAIM.c \
-o ./frictionAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/frictionAIM.so ./frictionAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
gfortran -g -c -O -fPIC -frecursive -fcray-pointer friction_eja_mod.f -o ./friction.o
gfortran -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/friction ./friction.o
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/friction'
make -C tetgen
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/tetgen'
g++ -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils tetgenAIM.cpp \
-o ./tetgenAIM.o
g++ -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I/home/jenkins/util/tetgen/tetgen1.6.0 -I../utils \
-DTETLIBRARY tetgen_Interface.cpp -o ./tetgen_Interface.o
g++ -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DTETLIBRARY -w /home/jenkins/util/tetgen/tetgen1.6.0/tetgen.cxx -o ./tetgen.o
g++ -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -O0 -w /home/jenkins/util/tetgen/tetgen1.6.0/predicates.cxx -o ./predicates.o
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tetgenAIM.so ./tetgenAIM.o \
./tetgen_Interface.o ./tetgen.o \
./predicates.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -ldl -lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/tetgen'
make -C tacs
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/tacs'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils tacsAIM.c \
-o ./tacsAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tacsAIM.so ./tacsAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/tacs'
make -C astros
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/astros'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils astrosAIM.c \
-o ./astrosAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils astrosUtils.c \
-o ./astrosUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils astrosCards.c \
-o ./astrosCards.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/astrosAIM.so ./astrosAIM.o ./astrosUtils.o ./astrosCards.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/astros'
make -C pointwise
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/pointwise'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils pointwiseAIM.c \
-o ./pointwiseAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils hashElement.c \
-o ./hashElement.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pointwiseAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pointwiseAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pointwiseAIM.so ./pointwiseAIM.o ./hashElement.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm -lpthread
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/pointwise'
make -C xfoil
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/xfoil'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils \
xfoilAIM.c -o ./xfoilAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/xfoilAIM.so ./xfoilAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/xfoil'
make -C aflr2
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/aflr2'
Not compiling aflr2AIM: AFLR must be set -- Please fix the environment....
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/aflr2'
make -C aflr4
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/aflr4'
Not compiling aflr4AIM: AFLR must be set -- Please fix the environment....
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/aflr4'
make -C su2
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/su2'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../meshWriter/su2Writer -I../utils su2AIM.c \
-o ./su2AIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils su2Utils.c \
-o ./su2Utils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils su2_4_Cardinal.c \
-o ./su2_4_Cardinal.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils su2_5_Raven.c \
-o ./su2_5_Raven.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils su2_6_Falcon.c \
-o ./su2_6_Falcon.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils su2_7_Blackbird.c \
-o ./su2_7_Blackbird.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils su2_801_Harrier.c \
-o ./su2_801_Harrier.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/su2AIM.so ./su2AIM.o ./su2Utils.o ./su2_4_Cardinal.o ./su2_5_Raven.o ./su2_6_Falcon.o ./su2_7_Blackbird.o ./su2_801_Harrier.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/su2'
make -C cgt
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/cgt'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include egads2cgt.c \
-o ./egads2cgt.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include aflr4egads.c \
-o ./aflr4egads.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/egads2cgt ./egads2cgt.o ./aflr4egads.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -legads -lcaps -locsm -lrt -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/cgt'
make -C mses
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/mses'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils msesAIM.c -o msesAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils msesUtils.c -o msesUtils.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/msesAIM.so ./msesAIM.o ./msesUtils.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/mses'
make -C egadsTess
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/egadsTess'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils egadsTessAIM.c \
-o ./egadsTessAIM.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/egadsTessAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/egadsTessAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/egadsTessAIM.so ./egadsTessAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/egadsTess'
make -C sierraSD
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/sierraSD'
Not compiling sierraSDAIM: SEACAS must be set -- Please fix the environment....
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/sierraSD'
make -C masstran
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/masstran'
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils masstranAIM.cpp \
-o ./masstranAIM.o
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/masstranAIM.so ./masstranAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/masstran'
make -C plato
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/plato'
Not compiling platoAIM: SEACAS must be set -- Please fix the environment....
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/plato'
make -C refine
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/refine'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/libmeshbWriter refineAIM.c \
-o ./refineAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 \
-I../meshWriter/libmeshbWriter/libMeshb/sources \
../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \
-o ./libmeshb7.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/refineAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/refineAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/refineAIM.so ./refineAIM.o ./libmeshb7.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/refine'
make -C awave
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/awave'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils awaveAIM.c \
-o ./awaveAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/awaveAIM.so ./awaveAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/awave'
make -C tsfoil
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/tsfoil'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils \
tsfoilAIM.c -o ./tsfoilAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tsfoilAIM.so ./tsfoilAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/tsfoil'
make -C delaundo
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/delaundo'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils delaundoAIM.c \
-o ./delaundoAIM.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/delaundoAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/delaundoAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/delaundoAIM.so ./delaundoAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/delaundo'
make -C abaqus
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/abaqus'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils \
abaqusAIM.c -o ./abaqusAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils \
abaqusUtils.c -o ./abaqusUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils \
-I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/abaqusFILReader.c -o ./abaqusFILReader.o
echo "Building Abaqus with Python"
Building Abaqus with Python
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/abaqusAIM.so ./abaqusAIM.o ./abaqusUtils.o ./abaqusFILReader.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lm -ldl -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/abaqus'
make -C fun3d
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/fun3d'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \
-I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython fun3dAIM.c -o ./fun3dAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \
fun3dUtils.c -o ./fun3dUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils \
-I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/fun3dNamelist.c -o ./fun3dNamelist.o
Building FUN3D with Python
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/fun3dAIM.so ./fun3dAIM.o ./fun3dUtils.o \
./fun3dNamelist.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -ldl -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lm -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/fun3d'
make -C cbaero
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/cbaero'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I. -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o cbaeroAIM.o
gcc -g -shared -Wl,-no-undefined cbaeroAIM.o -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/cbaeroAIM.so -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/cbaero'
make -C interference
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/interference'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include interferenceAIM.c \
-o ./interferenceAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. cloudFns.c \
-o ./cloudFns.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/interferenceAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/interferenceAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/interferenceAIM.so \
./interferenceAIM.o ./cloudFns.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib \
-laimUtil -locsm -legads -ludunits2 -ldl -lstdc++ -lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/interference'
make -C meshWriter
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter'
make -C libmeshbWriter
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/libmeshbWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include libmeshbWriter.c \
-o ./libmeshbWriter.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -IlibMeshb/sources -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include libMeshb/sources/libmeshb7.c \
-o ./libmeshb7.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libmeshbWriter.so ./libmeshbWriter.o ./libmeshb7.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/libmeshbWriter'
make -C fastWriter
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/fastWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include fastWriter.c \
-o ./fastWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/fastWriter.so ./fastWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/fastWriter'
make -C tecplotWriter
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/tecplotWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include tecplotWriter.c \
-o ./tecplotWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tecplotWriter.so ./tecplotWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/tecplotWriter'
make -C vtkWriter
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/vtkWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include vtkWriter.c \
-o ./vtkWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vtkWriter.so ./vtkWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/vtkWriter'
make -C bstlWriter
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bstlWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include bstlWriter.c \
-o ./bstlWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bstlWriter.so ./bstlWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bstlWriter'
make -C bvtkWriter
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bvtkWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include bvtkWriter.c \
-o ./bvtkWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bvtkWriter.so ./bvtkWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bvtkWriter'
make -C su2Writer
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/su2Writer'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include su2Writer.c \
-o ./su2Writer.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/su2Writer.so ./su2Writer.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/su2Writer'
make -C stlWriter
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/stlWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include stlWriter.c \
-o ./stlWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stlWriter.so ./stlWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/stlWriter'
make -C ugridWriter
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/ugridWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include ugridWriter.c \
-o ./ugridWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ugridWriter.so ./ugridWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/ugridWriter'
make -C exodusWriter
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/exodusWriter'
make[3]: Nothing to be done for 'default'.
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/exodusWriter'
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter'
make -C cart3d
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/cart3d'
make[2]: xml2-config: Command not found
XML developer libarary missing. Not compiling cart3dAIM.
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/cart3d'
make -C nastran
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/nastran'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils nastranAIM.c \
-o ./nastranAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nastranAIM.so ./nastranAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/nastran'
make -C spinnaker
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/spinnaker'
make[2]: Nothing to be done for 'default'.
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/spinnaker'
make -C aflr3
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/aflr3'
Not compiling aflr3AIM: AFLR must be set -- Please fix the environment....
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/aflr3'
make -C sierraSM
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/sierraSM'
Not compiling sierraSMAIM: SEACAS must be set -- Please fix the environment....
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/sierraSM'
make -C hsm
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils hsmAIM.c \
-o src/hsmAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils hsmUtils.c \
-o src/hsmUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils hsmAdj.c \
-o src/hsmAdj.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -Wno-comment rcm/rcm.cpp -DREVISION=7.7 \
-o src/rcm.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 rcm/genrcmi.cpp -DREVISION=7.7 \
-o src/genrcmi.o
make -C src hsmglr.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmglr.f -o ./hsmglr.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmbc.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbc.f -o ./hsmbc.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmbb2.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbb2.f -o ./hsmbb2.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmre1.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmre1.f -o ./hsmre1.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmdep.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmdep.f -o ./hsmdep.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmrfm.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmrfm.f -o ./hsmrfm.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmout.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmout.f -o ./hsmout.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmren.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmren.f -o ./hsmren.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmprj.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmprj.f -o ./hsmprj.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src atanc.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero atanc.f -o ./atanc.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src cross.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero cross.f -o ./cross.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src ludcmp.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero ludcmp.f -o ./ludcmp.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmabd.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmabd.f -o ./hsmabd.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src bmdump.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero bmdump.f -o ./bmdump.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmrun.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero -fno-recursive hsmrun.f -o ./hsmrun.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmeqn.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmeqn.f -o ./hsmeqn.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmsol.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmsol.f -o ./hsmsol.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmgeo.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmgeo.f -o ./hsmgeo.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src sbsolve.o
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero sbsolve.f -o ./sbsolve.o
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libhsm.a
make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libhsm.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libhsm.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libhsm.a hsmsol.o hsmdep.o hsmout.o hsmgeo.o hsmabd.o hsmeqn.o hsmbc.o hsmprj.o hsmren.o hsmre1.o hsmrfm.o hsmbb2.o hsmglr.o ludcmp.o sbsolve.o atanc.o bmdump.o cross.o )
ar: creating /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libhsm.a
make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/hsmAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/hsmAIM.so
gfortran -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/hsmAIM.so \
src/hsmAIM.o src/hsmUtils.o src/hsmAdj.o \
src/rcm.o src/genrcmi.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -lhsm -ldl -lstdc++
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm'
make -C avl
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/avl'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils avlAIM.c -o ./avlAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o avlRead_ELE.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o avlRead_DERMATB.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o avlRead_HINGE.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o avlRead_BODY.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o avlRead_CNC.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o avlRead_TOT.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o avlRead_DERMATS.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o avlRead_STRP.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o avlRead_VM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o avlRead_CPOML.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o avlRead_DERMATM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o avlRead_SURF.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/avlAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/avlAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/avlAIM.so ./avlAIM.o ./avlRead_ELE.o ./avlRead_DERMATB.o ./avlRead_HINGE.o ./avlRead_BODY.o ./avlRead_CNC.o ./avlRead_TOT.o ./avlRead_DERMATS.o ./avlRead_STRP.o ./avlRead_VM.o ./avlRead_CPOML.o ./avlRead_DERMATM.o ./avlRead_SURF.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \
-lstdc++ -lrt -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/avl'
make -C custom
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/custom'
make[2]: Nothing to be done for 'default'.
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/custom'
make -C skeleton
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/skeleton'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils skeletonAIM.c \
-o ./skeletonAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/skeletonAIM.so ./skeletonAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/skeleton'
make -C unitTest
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest'
make[2]: Nothing to be done for 'all'.
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest'
make -C mystran
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/mystran'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils mystranAIM.c \
-o ./mystranAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils mystranUtils.c \
-o ./mystranUtils.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mystranAIM.so ./mystranAIM.o ./mystranUtils.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/mystran'
make -C zaero
make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/zaero'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils zaeroAIM.c -o zaeroAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils zaeroUtils.c -o zaeroUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils zaeroLinearFlutter.c -o zaeroLinearFlutter.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils zaeroTrim.c -o zaeroTrim.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils zaeroTypes.c -o zaeroTypes.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils zaeroCards.c -o zaeroCards.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils zaeroGeneral.c -o zaeroGeneral.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils zaeroGraphical.c -o zaeroGraphical.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/zaeroAIM.so ./zaeroAIM.o ./zaeroUtils.o ./zaeroLinearFlutter.o ./zaeroTrim.o ./zaeroTypes.o ./zaeroCards.o ./zaeroGeneral.o ./zaeroGraphical.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/zaero'
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim'
(cd OpenCSM; make -f serveESP.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/OpenCSM'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timCapsMode.c -o ./timCapsMode.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/capsMode.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/capsMode.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/capsMode.so ./timCapsMode.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timFlowchart.c -o ./timFlowchart.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/flowchart.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/flowchart.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/flowchart.so ./timFlowchart.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timViewer.c -o ./timViewer.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/viewer.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/viewer.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/viewer.so ./timViewer.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 timPyscript.c -o ./timPyscript.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pyscript.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pyscript.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pyscript.so ./timPyscript.o -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lrt -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/OpenCSM'
*** Build Completed! ***
+ export CSMDATA=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data
+ CSMDATA=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin
++ uname -a
+ [[ Linux reynolds-centOS8 4.18.0-552.el8.x86_64 #1 SMP Sun Apr 7 19:39:51 UTC 2024 x86_64 x86_64 x86_64 GNU/Linux == *\D\a\r\w\i\n* ]]
+ sed -i 's/.*capsExamples.*/#&/' /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/Verification.sh
+ bash -ex /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/Verification.sh
+ expectSuccess 01 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/expressions.vfy", so verification is being skipped
ERROR:: 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 0m0.112s
user 0m0.090s
sys 0m0.020s
+ set +x
=============================================
ESP verification case 01 passed (as expected)
=============================================
+ expectSuccess 02 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/demo2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/demo2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/demo2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.408s
user 0m0.558s
sys 0m0.038s
+ set +x
=============================================
ESP verification case 02 passed (as expected)
=============================================
+ expectSuccess 03 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/tutorial1_whole
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/tutorial1_whole
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/verify_7.7.0/tutorial1_whole.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m2.704s
user 0m4.415s
sys 0m0.148s
+ set +x
=============================================
ESP verification case 03 passed (as expected)
=============================================
+ expectSuccess 04 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/design2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/design2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/design2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.626s
user 0m0.813s
sys 0m0.030s
+ set +x
=============================================
ESP verification case 04 passed (as expected)
=============================================
+ expectSuccess 05 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/design3
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/design3
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/design3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.499s
user 0m0.866s
sys 0m0.021s
+ set +x
=============================================
ESP verification case 05 passed (as expected)
=============================================
+ expectSuccess 06 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/tutorial2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/tutorial2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/verify_7.7.0/tutorial2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.493s
user 0m0.854s
sys 0m0.026s
+ set +x
=============================================
ESP verification case 06 passed (as expected)
=============================================
+ expectSuccess 07 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/tutorial3
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/tutorial3
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/verify_7.7.0/tutorial3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m3.484s
user 0m5.828s
sys 0m0.105s
+ set +x
=============================================
ESP verification case 07 passed (as expected)
=============================================
+ expectSuccess 08 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/CAPS/myPlane
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/CAPS/myPlane
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/CAPS/verify_7.7.0/myPlane.vfy", so verification is being skipped
==> serveESP completed successfully with 12 warnings and no verification data
real 0m27.640s
user 0m46.468s
sys 0m0.338s
+ set +x
=============================================
ESP verification case 08 passed (as expected)
=============================================
+ expectSuccess 09 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/bottle
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/bottle
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/verify_7.7.0/bottle.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.642s
user 0m0.639s
sys 0m0.018s
+ set +x
=============================================
ESP verification case 09 passed (as expected)
=============================================
+ expectSuccess 10 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/wingMultiModel
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/wingMultiModel
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/wingMultiModel.vfy", so verification is being skipped
==> serveESP completed successfully with 4 warnings and no verification data
real 0m34.136s
user 1m0.555s
sys 0m1.101s
+ set +x
=============================================
ESP verification case 10 passed (as expected)
=============================================
+ expectSuccess 11 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/bullet
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/bullet
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/bullet.vfy", so verification is being skipped
WARNING:: 8 _hist and/or __trace__ attributes removed
WARNING:: 8 _hist and/or __trace__ attributes removed
==> serveESP completed successfully with 1 warnings and no verification data
real 0m0.341s
user 0m0.390s
sys 0m0.026s
+ set +x
=============================================
ESP verification case 11 passed (as expected)
=============================================
+ expectSuccess 12 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/connect5
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/connect5
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/connect5.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.644s
user 0m0.981s
sys 0m0.022s
+ set +x
=============================================
ESP verification case 12 passed (as expected)
=============================================
+ expectSuccess 13 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/group2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/group2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/group2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.182s
user 0m0.269s
sys 0m0.031s
+ set +x
=============================================
ESP verification case 13 passed (as expected)
=============================================
+ expectSuccess 14 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/csm3
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/csm3
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/csm3.vfy", so verification is being skipped
nnode=8
nedge=12
nface=6
nnode=8
nedge=12
nface=6
nnode=16
nedge=24
nface=10
nnode=8
nedge=12
nface=6
==> serveESP completed successfully with no verification data
real 0m0.453s
user 0m0.700s
sys 0m0.025s
+ set +x
=============================================
ESP verification case 14 passed (as expected)
=============================================
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/testEGADS
+ make test
python --version
Python 3.11.9
python -u -m unittest discover
.................................................... PCurve Map: 48 (alloc 48)!
Surface Map: 12 (alloc 24)!
Curve Map: 28 (alloc 28)!
Writing PCurves...
Writing Curves...
Writing Surfaces...
Writing 16 Nodes...
Writing 28 Edges...
Writing 12 Loops...
Writing 12 Faces...
Writing 1 Shells...
EGADS Info: 0 Objects, 0 Reference in Use (of 972) at Close!
...................
----------------------------------------------------------------------
Ran 71 tests in 2.390s
OK
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/testOCSM
+ source /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/JenkinsESP/test_pyOCSM.sh
++ set -x
++ python -u test_pyOCSM.py -skipHelp
real 0m5.452s
user 0m10.014s
sys 0m0.110s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/testCAPS
+ make test
python --version
Python 3.11.9
python -u -m unittest discover
..Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing1, index = 1
Name = Wing2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 143
Number of elements = 282
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 282
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 140
Number of elements = 276
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 276
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 283
Combined Number of elements = 558
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 558
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Wing1
Property name - Wing2
Done getting FEA properties
Updating mesh element types based on properties input
... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
..Writing D3 Javascript library - d3.v3.min.js
........... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing1, index = 1
Name = Wing2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 209
Number of elements = 414
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 414
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 186
Number of elements = 368
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 368
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 395
Combined Number of elements = 782
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 782
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Wing1
Property name - Wing2
Done getting FEA properties
Updating mesh element types based on properties input
..........--> Opening DESPMTR file "unitGeom.param"
updating CFGPMTR series [ 1, 1] = 8412.000000
updating CFGPMTR series2 [ 1, 1] = 20.000000
updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000
updating CFGPMTR nrow [ 1, 1] = 3.000000
updating CFGPMTR ncol [ 1, 1] = 2.000000
updating DESPMTR area [ 1, 1] = 40.000000
updating DESPMTR aspect [ 1, 1] = 5.000000
updating DESPMTR taper [ 1, 1] = 0.500000
updating DESPMTR twist [ 1, 1] = 15.000000
updating DESPMTR wing:lesweep [ 1, 1] = 30.000000
updating DESPMTR wing:dihedral [ 1, 1] = 1.000000
updating DESPMTR wing:chord:root [ 1, 1] = 1.560000
updating DESPMTR htail [ 1, 1] = 1.000000
updating DESPMTR htail:chord [ 1, 1] = 2.000000
updating DESPMTR vtail:chord [ 1, 1] = 3.000000
updating DESPMTR vtail [ 1, 1] = 4.000000
updating DESPMTR sphereR [ 1, 1] = 80.000000
updating DESPMTR v@1:d_name [ 1, 1] = 1.000000
updating DESPMTR despMat [ 1, 1] = 11.000000
updating DESPMTR despMat [ 1, 2] = 12.000000
updating DESPMTR despMat [ 2, 1] = 13.000000
updating DESPMTR despMat [ 2, 2] = 14.000000
updating DESPMTR despMat [ 3, 1] = 15.000000
updating DESPMTR despMat [ 3, 2] = 16.000000
updating DESPMTR despCol [ 1, 1] = 11.000000
updating DESPMTR despCol [ 2, 1] = 13.000000
updating DESPMTR despCol [ 3, 1] = 15.000000
updating DESPMTR despRow [ 1, 1] = 11.000000
updating DESPMTR despRow [ 1, 2] = 12.000000
updating DESPMTR despRow [ 1, 3] = 13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
..Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
No linkable data found for Altitude
No linkable data found for Strings
No linkable data found for Strings2
Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
............ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. CAPS Info: Hit last success -- going live!
... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.--> Opening DESPMTR file "unitGeom.param"
updating CFGPMTR series [ 1, 1] = 8412.000000
updating CFGPMTR series2 [ 1, 1] = 20.000000
updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000
updating CFGPMTR nrow [ 1, 1] = 3.000000
updating CFGPMTR ncol [ 1, 1] = 2.000000
updating DESPMTR area [ 1, 1] = 40.000000
updating DESPMTR aspect [ 1, 1] = 5.000000
updating DESPMTR taper [ 1, 1] = 0.500000
updating DESPMTR twist [ 1, 1] = 15.000000
updating DESPMTR wing:lesweep [ 1, 1] = 30.000000
updating DESPMTR wing:dihedral [ 1, 1] = 1.000000
updating DESPMTR wing:chord:root [ 1, 1] = 1.560000
updating DESPMTR htail [ 1, 1] = 1.000000
updating DESPMTR htail:chord [ 1, 1] = 2.000000
updating DESPMTR vtail:chord [ 1, 1] = 3.000000
updating DESPMTR vtail [ 1, 1] = 4.000000
updating DESPMTR sphereR [ 1, 1] = 80.000000
updating DESPMTR v@1:d_name [ 1, 1] = 1.000000
updating DESPMTR despMat [ 1, 1] = 11.000000
updating DESPMTR despMat [ 1, 2] = 12.000000
updating DESPMTR despMat [ 2, 1] = 13.000000
updating DESPMTR despMat [ 2, 2] = 14.000000
updating DESPMTR despMat [ 3, 1] = 15.000000
updating DESPMTR despMat [ 3, 2] = 16.000000
updating DESPMTR despCol [ 1, 1] = 11.000000
updating DESPMTR despCol [ 2, 1] = 13.000000
updating DESPMTR despCol [ 3, 1] = 15.000000
updating DESPMTR despRow [ 1, 1] = 11.000000
updating DESPMTR despRow [ 1, 2] = 12.000000
updating DESPMTR despRow [ 1, 3] = 13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
................ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
----------------------------------------------------------------------
Ran 100 tests in 13.343s
OK
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/
+ make test
python --version
Python 3.11.9
python -u -m unittest discover --verbose
Please set the environment variable ASTROS_ROOT
test_journal (test_aflr2.TestAFLR2.test_journal) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 04/23/24 @ 12:17PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2244 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2244 2244
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 450 902
AFLR2 IG : Nodes, Faces = 900 1802
AFLR2 IG : Nodes, Faces = 1145 2292
AFLR2 IG : Nodes, Faces = 1260 2522
AFLR2 IG : Nodes, Faces = 1350 2702
AFLR2 IG : Nodes, Faces = 1360 2722
AFLR2 IG : Nodes, Faces = 1460 2922
AFLR2 IG : Nodes, Faces = 1560 3122
AFLR2 IG : Nodes, Faces = 1660 3322
AFLR2 IG : Nodes, Faces = 1760 3522
AFLR2 IG : Nodes, Faces = 1800 3602
AFLR2 IG : Nodes, Faces = 1860 3722
AFLR2 IG : Nodes, Faces = 1960 3922
AFLR2 IG : Nodes, Faces = 2060 4122
AFLR2 IG : Nodes, Faces = 2085 4172
AFLR2 IG : Nodes, Faces = 2244 4490
AFLR2 IG : Nodes, Faces = 2248 4490
AFLR2 IG : Nodes, Faces = 2244 2244
AFLR2 : CPU Time = 0.039 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 = 0.124 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
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 = 0.048 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 = 0.127 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.008 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 = 0.075 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2244 2244
AFLR2 GG : Nodes, Faces = 4283 6322
AFLR2 GG : Nodes, Faces = 6128 10012
AFLR2 GG : Nodes, Faces = 7863 13482
AFLR2 GG : Nodes, Faces = 9464 16684
AFLR2 GG : Nodes, Faces = 10948 19652
AFLR2 GG : Nodes, Faces = 12322 22400
AFLR2 GG : Nodes, Faces = 13619 24994
AFLR2 GG : Nodes, Faces = 14829 27414
AFLR2 GG : Nodes, Faces = 15981 29718
AFLR2 GG : Nodes, Faces = 17082 31920
AFLR2 GG : Nodes, Faces = 18110 33976
AFLR2 GG : Nodes, Faces = 19081 35918
AFLR2 GG : Nodes, Faces = 20014 37784
AFLR2 GG : Nodes, Faces = 20924 39604
AFLR2 GG : Nodes, Faces = 21782 41320
AFLR2 GG : Nodes, Faces = 22595 42946
AFLR2 GG : Nodes, Faces = 23377 44510
AFLR2 GG : Nodes, Faces = 24129 46014
AFLR2 GG : Nodes, Faces = 24840 47436
AFLR2 GG : Nodes, Faces = 25522 48800
AFLR2 GG : Nodes, Faces = 26170 50096
AFLR2 GG : Nodes, Faces = 26793 51342
AFLR2 GG : Nodes, Faces = 27346 52448
AFLR2 GG : Nodes, Faces = 27846 53448
AFLR2 GG : Nodes, Faces = 28280 54316
AFLR2 GG : Nodes, Faces = 28652 55060
AFLR2 GG : Nodes, Faces = 28920 55596
AFLR2 GG : Nodes, Faces = 29143 56042
AFLR2 GG : Nodes, Faces = 29358 56472
AFLR2 GG : Nodes, Faces = 29550 56856
AFLR2 GG : Nodes, Faces = 29693 57142
AFLR2 GG : Nodes, Faces = 29805 57366
AFLR2 GG : Nodes, Faces = 29875 57506
AFLR2 GG : Nodes, Faces = 29895 57546
AFLR2 GG : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.122 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.009 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
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 = 0.061 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 = 0.125 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.025 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
ok
test_phase (test_aflr2.TestAFLR2.test_phase) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2244 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2244 2244
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 450 902
AFLR2 IG : Nodes, Faces = 900 1802
AFLR2 IG : Nodes, Faces = 1145 2292
AFLR2 IG : Nodes, Faces = 1260 2522
AFLR2 IG : Nodes, Faces = 1350 2702
AFLR2 IG : Nodes, Faces = 1360 2722
AFLR2 IG : Nodes, Faces = 1460 2922
AFLR2 IG : Nodes, Faces = 1560 3122
AFLR2 IG : Nodes, Faces = 1660 3322
AFLR2 IG : Nodes, Faces = 1760 3522
AFLR2 IG : Nodes, Faces = 1800 3602
AFLR2 IG : Nodes, Faces = 1860 3722
AFLR2 IG : Nodes, Faces = 1960 3922
AFLR2 IG : Nodes, Faces = 2060 4122
AFLR2 IG : Nodes, Faces = 2085 4172
AFLR2 IG : Nodes, Faces = 2244 4490
AFLR2 IG : Nodes, Faces = 2248 4490
AFLR2 IG : Nodes, Faces = 2244 2244
AFLR2 : CPU Time = 0.032 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2244 2244
AFLR2 GG : Nodes, Faces = 4283 6322
AFLR2 GG : Nodes, Faces = 6128 10012
AFLR2 GG : Nodes, Faces = 7863 13482
AFLR2 GG : Nodes, Faces = 9464 16684
AFLR2 GG : Nodes, Faces = 10948 19652
AFLR2 GG : Nodes, Faces = 12322 22400
AFLR2 GG : Nodes, Faces = 13619 24994
AFLR2 GG : Nodes, Faces = 14829 27414
AFLR2 GG : Nodes, Faces = 15981 29718
AFLR2 GG : Nodes, Faces = 17082 31920
AFLR2 GG : Nodes, Faces = 18110 33976
AFLR2 GG : Nodes, Faces = 19081 35918
AFLR2 GG : Nodes, Faces = 20014 37784
AFLR2 GG : Nodes, Faces = 20924 39604
AFLR2 GG : Nodes, Faces = 21782 41320
AFLR2 GG : Nodes, Faces = 22595 42946
AFLR2 GG : Nodes, Faces = 23377 44510
AFLR2 GG : Nodes, Faces = 24129 46014
AFLR2 GG : Nodes, Faces = 24840 47436
AFLR2 GG : Nodes, Faces = 25522 48800
AFLR2 GG : Nodes, Faces = 26170 50096
AFLR2 GG : Nodes, Faces = 26793 51342
AFLR2 GG : Nodes, Faces = 27346 52448
AFLR2 GG : Nodes, Faces = 27846 53448
AFLR2 GG : Nodes, Faces = 28280 54316
AFLR2 GG : Nodes, Faces = 28652 55060
AFLR2 GG : Nodes, Faces = 28920 55596
AFLR2 GG : Nodes, Faces = 29143 56042
AFLR2 GG : Nodes, Faces = 29358 56472
AFLR2 GG : Nodes, Faces = 29550 56856
AFLR2 GG : Nodes, Faces = 29693 57142
AFLR2 GG : Nodes, Faces = 29805 57366
AFLR2 GG : Nodes, Faces = 29875 57506
AFLR2 GG : Nodes, Faces = 29895 57546
AFLR2 GG : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.106 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.009 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 48 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 48 48
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 10 22
AFLR2 IG : Nodes, Faces = 20 42
AFLR2 IG : Nodes, Faces = 30 62
AFLR2 IG : Nodes, Faces = 40 82
AFLR2 IG : Nodes, Faces = 45 92
AFLR2 IG : Nodes, Faces = 46 94
AFLR2 IG : Nodes, Faces = 48 98
AFLR2 IG : Nodes, Faces = 52 98
AFLR2 IG : Nodes, Faces = 48 48
AFLR2 : CPU Time = 0.000 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 48 48
AFLR2 GG : Nodes, Faces = 88 128
AFLR2 GG : Nodes, Faces = 109 170
AFLR2 GG : Nodes, Faces = 124 200
AFLR2 GG : Nodes, Faces = 136 224
AFLR2 GG : Nodes, Faces = 148 248
AFLR2 GG : Nodes, Faces = 161 274
AFLR2 GG : Nodes, Faces = 171 294
AFLR2 GG : Nodes, Faces = 181 314
AFLR2 GG : Nodes, Faces = 187 326
AFLR2 GG : Nodes, Faces = 190 332
AFLR2 : CPU Time = 0.000 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 190 332
AFLR2 : CPU Time = 0.000 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 190
Number of elements = 380
Number of tris = 332
Number of quad = 0
ok
test_reenter (test_aflr2.TestAFLR2.test_reenter) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 339 680
AFLR2 IG : Nodes, Faces = 340 682
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.002 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 = 0.023 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 4705 9066
AFLR2 : CPU Time = 0.002 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 4705
Number of elements = 9410
Number of tris = 9066
Number of quad = 0
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates!
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 339 680
AFLR2 IG : Nodes, Faces = 340 682
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.001 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 344 344
AFLR2 GGp: Nodes, Faces = 682 1020
AFLR2 GGp: Nodes, Faces = 1010 1676
AFLR2 GGp: Nodes, Faces = 1316 2288
AFLR2 GGp: Nodes, Faces = 1592 2840
AFLR2 GGp: Nodes, Faces = 1855 3366
AFLR2 GGp: Nodes, Faces = 2106 3868
AFLR2 GGp: Nodes, Faces = 2341 4338
AFLR2 GGp: Nodes, Faces = 2551 4758
AFLR2 GGp: Nodes, Faces = 2741 5138
AFLR2 GGp: Nodes, Faces = 2917 5490
AFLR2 GGp: Nodes, Faces = 3082 5820
AFLR2 GGp: Nodes, Faces = 3240 6136
AFLR2 GGp: Nodes, Faces = 3379 6414
AFLR2 GGp: Nodes, Faces = 3513 6682
AFLR2 GGp: Nodes, Faces = 3642 6940
AFLR2 GGp: Nodes, Faces = 3748 7152
AFLR2 GGp: Nodes, Faces = 3846 7348
AFLR2 GGp: Nodes, Faces = 3931 7518
AFLR2 GGp: Nodes, Faces = 3999 7654
AFLR2 GGp: Nodes, Faces = 4044 7744
AFLR2 GGp: Nodes, Faces = 4058 7772
AFLR2 : CPU Time = 0.013 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 4058 7772
AFLR2 QI : Nodes, Faces = 4057 364
AFLR2 QI : Nodes, Faces = 4057 3703
AFLR2 QI : Nodes, Faces = 4057 7770
AFLR2 QI : Nodes, Faces = 4056 344
AFLR2 QI : Nodes, Faces = 4056 3712
AFLR2 QI : Nodes, Faces = 4056 7768
AFLR2 QI : Nodes, Faces = 4055 348
AFLR2 QI : Nodes, Faces = 4055 3709
AFLR2 QI : Nodes, Faces = 4055 7766
AFLR2 QI : Nodes, Faces = 4055 392
AFLR2 QI : Nodes, Faces = 4055 3687
AFLR2 QI : Nodes, Faces = 4055 7766
AFLR2 QI : Nodes, Faces = 4055 386
AFLR2 QI : Nodes, Faces = 4055 3690
AFLR2 QI : Nodes, Faces = 4055 386
AFLR2 QI : Nodes, Faces = 4055 3690
AFLR2 : CPU Time = 0.007 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 4055
Number of elements = 4420
Number of tris = 386
Number of quad = 3690
Writing 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 = 0.002 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 = 0.028 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 = 0.013 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:62030)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box, index = 1
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 04/23/24 @ 12:17PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR4 : Compile Date 04/23/24 @ 12:17PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 7):
Number of nodes = 1189
Number of elements = 6249
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4917
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cylinder, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 7):
Number of nodes = 6281
Number of elements = 34888
Number of triangles = 4448
Number of quadrilatarals = 0
Number of tetrahedrals = 30440
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cone, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 7):
Number of nodes = 13612
Number of elements = 76381
Number of triangles = 8144
Number of quadrilatarals = 0
Number of tetrahedrals = 68237
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = torus, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 7):
Number of nodes = 41953
Number of elements = 238379
Number of triangles = 19880
Number of quadrilatarals = 0
Number of tetrahedrals = 218499
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = sphere, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 7):
Number of nodes = 4364
Number of elements = 24190
Number of triangles = 3016
Number of quadrilatarals = 0
Number of tetrahedrals = 21174
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = boxhole, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 7):
Number of nodes = 11063
Number of elements = 61143
Number of triangles = 8630
Number of quadrilatarals = 0
Number of tetrahedrals = 52513
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = bullet, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 7):
Number of nodes = 10571
Number of elements = 59256
Number of triangles = 6368
Number of quadrilatarals = 0
Number of tetrahedrals = 52888
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Getting volume mesh for body 1 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 89033
Number of elements = 500486
Number of triangles = 51818
Number of quadrilatarals = 0
Number of tetrahedrals = 448668
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_all (test_aflr3.TestAFLR3.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = farfield, index = 8
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = farfield, index = 8
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 16433
Number of elements = 93529
Number of triangles = 7926
Number of quadrilatarals = 0
Number of tetrahedrals = 85603
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_box (test_aflr3.TestAFLR3.test_box) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2589
Number of elements = 13809
Number of triangles = 2758
Number of quadrilatarals = 0
Number of tetrahedrals = 11051
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_boxhole (test_aflr3.TestAFLR3.test_boxhole) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3645
Number of elements = 19765
Number of triangles = 3394
Number of quadrilatarals = 0
Number of tetrahedrals = 16371
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_bullet (test_aflr3.TestAFLR3.test_bullet) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5471
Number of elements = 30418
Number of triangles = 3656
Number of quadrilatarals = 0
Number of tetrahedrals = 26762
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_cone (test_aflr3.TestAFLR3.test_cone) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4694
Number of elements = 25935
Number of triangles = 3326
Number of quadrilatarals = 0
Number of tetrahedrals = 22609
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_cylinder (test_aflr3.TestAFLR3.test_cylinder) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5554
Number of elements = 30862
Number of triangles = 3756
Number of quadrilatarals = 0
Number of tetrahedrals = 27106
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_faceMatch (test_aflr3.TestAFLR3.test_faceMatch) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2260
Number of elements = 12133
Number of triangles = 2222
Number of quadrilatarals = 0
Number of tetrahedrals = 9911
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2392
Number of elements = 12577
Number of triangles = 2666
Number of quadrilatarals = 0
Number of tetrahedrals = 9911
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3341
Number of elements = 18069
Number of triangles = 3110
Number of quadrilatarals = 0
Number of tetrahedrals = 14959
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3606
Number of elements = 18961
Number of triangles = 4002
Number of quadrilatarals = 0
Number of tetrahedrals = 14959
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4414
Number of elements = 23974
Number of triangles = 3998
Number of quadrilatarals = 0
Number of tetrahedrals = 19976
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4811
Number of elements = 25310
Number of triangles = 5334
Number of quadrilatarals = 0
Number of tetrahedrals = 19976
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 4):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 4):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 4):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 4):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5490
Number of elements = 29891
Number of triangles = 4886
Number of quadrilatarals = 0
Number of tetrahedrals = 25005
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6019
Number of elements = 31671
Number of triangles = 6666
Number of quadrilatarals = 0
Number of tetrahedrals = 25005
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 5):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 5):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 5):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 5):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 5):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6542
Number of elements = 35667
Number of triangles = 5774
Number of quadrilatarals = 0
Number of tetrahedrals = 29893
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 7203
Number of elements = 37891
Number of triangles = 7998
Number of quadrilatarals = 0
Number of tetrahedrals = 29893
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 6):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 6):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 6):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 6):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 6):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 6):
Number of nodes = 1184
Number of elements = 6220
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4888
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 7601
Number of elements = 41489
Number of triangles = 6662
Number of quadrilatarals = 0
Number of tetrahedrals = 34827
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8394
Number of elements = 44157
Number of triangles = 9330
Number of quadrilatarals = 0
Number of tetrahedrals = 34827
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 7):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 7):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 7):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 7):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 7):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 7):
Number of nodes = 1184
Number of elements = 6220
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4888
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 7):
Number of nodes = 1191
Number of elements = 6266
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4934
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 19800
Number of elements = 109798
Number of triangles = 15540
Number of quadrilatarals = 0
Number of tetrahedrals = 94258
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 8 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 9 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 10 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 11 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 12 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 13 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 14 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 15 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 16 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 17 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 18 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 19 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 22741
Number of elements = 119570
Number of triangles = 25312
Number of quadrilatarals = 0
Number of tetrahedrals = 94258
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 19):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 19):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 19):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 19):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 19):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 19):
Number of nodes = 1184
Number of elements = 6220
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4888
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 19):
Number of nodes = 1191
Number of elements = 6266
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4934
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 8 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 8 (of 19):
Number of nodes = 1193
Number of elements = 6272
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4940
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 9 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 9 (of 19):
Number of nodes = 1176
Number of elements = 6165
Number of triangles = 1330
Number of quadrilatarals = 0
Number of tetrahedrals = 4835
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 10 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 10 (of 19):
Number of nodes = 1203
Number of elements = 6314
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4982
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 11 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 11 (of 19):
Number of nodes = 1192
Number of elements = 6269
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4937
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 12 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 12 (of 19):
Number of nodes = 1192
Number of elements = 6269
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4937
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 13 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 13 (of 19):
Number of nodes = 1198
Number of elements = 6296
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4964
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 14 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 14 (of 19):
Number of nodes = 1223
Number of elements = 6443
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5111
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 15 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 15 (of 19):
Number of nodes = 1184
Number of elements = 6224
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4892
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 16 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 16 (of 19):
Number of nodes = 1195
Number of elements = 6287
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4955
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 17 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 17 (of 19):
Number of nodes = 1197
Number of elements = 6311
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4979
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 18 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 18 (of 19):
Number of nodes = 1203
Number of elements = 6310
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4978
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 19 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 19 (of 19):
Number of nodes = 1191
Number of elements = 6253
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4921
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_faceMatch_MultiDomain (test_aflr3.TestAFLR3.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8857
Number of elements = 49191
Number of triangles = 6284
Number of quadrilatarals = 0
Number of tetrahedrals = 42907
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8989
Number of elements = 49635
Number of triangles = 6728
Number of quadrilatarals = 0
Number of tetrahedrals = 42907
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 7796
Number of elements = 43368
Number of triangles = 5396
Number of quadrilatarals = 0
Number of tetrahedrals = 37972
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 1193
Number of elements = 6267
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4935
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9944
Number of elements = 55193
Number of triangles = 7174
Number of quadrilatarals = 0
Number of tetrahedrals = 48019
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10218
Number of elements = 56081
Number of triangles = 8062
Number of quadrilatarals = 0
Number of tetrahedrals = 48019
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7818
Number of elements = 43469
Number of triangles = 5398
Number of quadrilatarals = 0
Number of tetrahedrals = 38071
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1202
Number of elements = 6320
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4988
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 1198
Number of elements = 6292
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4960
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9609
Number of elements = 53228
Number of triangles = 6994
Number of quadrilatarals = 0
Number of tetrahedrals = 46234
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9829
Number of elements = 53956
Number of triangles = 7722
Number of quadrilatarals = 0
Number of tetrahedrals = 46234
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7789
Number of elements = 43295
Number of triangles = 5394
Number of quadrilatarals = 0
Number of tetrahedrals = 37901
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1186
Number of elements = 6230
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4898
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 854
Number of elements = 4431
Number of triangles = 996
Number of quadrilatarals = 0
Number of tetrahedrals = 3435
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9348
Number of elements = 51734
Number of triangles = 6812
Number of quadrilatarals = 0
Number of tetrahedrals = 44922
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9531
Number of elements = 52330
Number of triangles = 7408
Number of quadrilatarals = 0
Number of tetrahedrals = 44922
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7804
Number of elements = 43358
Number of triangles = 5386
Number of quadrilatarals = 0
Number of tetrahedrals = 37972
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1200
Number of elements = 6311
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4979
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 527
Number of elements = 2661
Number of triangles = 690
Number of quadrilatarals = 0
Number of tetrahedrals = 1971
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9183
Number of elements = 50871
Number of triangles = 6632
Number of quadrilatarals = 0
Number of tetrahedrals = 44239
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9322
Number of elements = 51307
Number of triangles = 7068
Number of quadrilatarals = 0
Number of tetrahedrals = 44239
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7927
Number of elements = 44116
Number of triangles = 5382
Number of quadrilatarals = 0
Number of tetrahedrals = 38734
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 868
Number of elements = 4530
Number of triangles = 996
Number of quadrilatarals = 0
Number of tetrahedrals = 3534
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 527
Number of elements = 2661
Number of triangles = 690
Number of quadrilatarals = 0
Number of tetrahedrals = 1971
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10181
Number of elements = 56797
Number of triangles = 6782
Number of quadrilatarals = 0
Number of tetrahedrals = 50015
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10671
Number of elements = 58561
Number of triangles = 8546
Number of quadrilatarals = 0
Number of tetrahedrals = 50015
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7741
Number of elements = 43010
Number of triangles = 5362
Number of quadrilatarals = 0
Number of tetrahedrals = 37648
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 2692
Number of elements = 14435
Number of triangles = 2800
Number of quadrilatarals = 0
Number of tetrahedrals = 11635
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 238
Number of elements = 1116
Number of triangles = 384
Number of quadrilatarals = 0
Number of tetrahedrals = 732
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1500
Number of elements = 7757
Number of triangles = 1986
Number of quadrilatarals = 0
Number of tetrahedrals = 5771
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1564
Number of elements = 7881
Number of triangles = 2110
Number of quadrilatarals = 0
Number of tetrahedrals = 5771
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 1160
Number of elements = 6087
Number of triangles = 1308
Number of quadrilatarals = 0
Number of tetrahedrals = 4779
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 360
Number of elements = 1635
Number of triangles = 718
Number of quadrilatarals = 0
Number of tetrahedrals = 917
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 44
Number of elements = 159
Number of triangles = 84
Number of quadrilatarals = 0
Number of tetrahedrals = 75
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5077
Number of elements = 27808
Number of triangles = 4070
Number of quadrilatarals = 0
Number of tetrahedrals = 23738
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5223
Number of elements = 28360
Number of triangles = 4622
Number of quadrilatarals = 0
Number of tetrahedrals = 23738
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 4887
Number of elements = 26853
Number of triangles = 4038
Number of quadrilatarals = 0
Number of tetrahedrals = 22815
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 336
Number of elements = 1507
Number of triangles = 584
Number of quadrilatarals = 0
Number of tetrahedrals = 923
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 33090
Number of elements = 191624
Number of triangles = 8496
Number of quadrilatarals = 0
Number of tetrahedrals = 183128
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 36430
Number of elements = 204952
Number of triangles = 21824
Number of quadrilatarals = 0
Number of tetrahedrals = 183128
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 5):
Number of nodes = 28936
Number of elements = 164394
Number of triangles = 15160
Number of quadrilatarals = 0
Number of tetrahedrals = 149234
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 5):
Number of nodes = 1415
Number of elements = 7515
Number of triangles = 1456
Number of quadrilatarals = 0
Number of tetrahedrals = 6059
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 5):
Number of nodes = 4115
Number of elements = 22780
Number of triangles = 2940
Number of quadrilatarals = 0
Number of tetrahedrals = 19840
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 5):
Number of nodes = 711
Number of elements = 3685
Number of triangles = 844
Number of quadrilatarals = 0
Number of tetrahedrals = 2841
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 5):
Number of nodes = 1253
Number of elements = 6578
Number of triangles = 1424
Number of quadrilatarals = 0
Number of tetrahedrals = 5154
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 16800
Number of elements = 95304
Number of triangles = 8802
Number of quadrilatarals = 0
Number of tetrahedrals = 86502
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 18724
Number of elements = 102680
Number of triangles = 16178
Number of quadrilatarals = 0
Number of tetrahedrals = 86502
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 12168
Number of elements = 68392
Number of triangles = 7142
Number of quadrilatarals = 0
Number of tetrahedrals = 61250
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 6556
Number of elements = 34288
Number of triangles = 9036
Number of quadrilatarals = 0
Number of tetrahedrals = 25252
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_journal (test_aflr3.TestAFLR3.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2940
Number of elements = 12771
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7319
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2497
Number of elements = 10947
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6395
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2940
Number of elements = 12771
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7319
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2497
Number of elements = 10947
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6395
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
ok
test_phase (test_aflr3.TestAFLR3.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2940
Number of elements = 12771
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7319
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2497
Number of elements = 10947
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6395
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_reenter (test_aflr3.TestAFLR3.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2940
Number of elements = 12771
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7319
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2497
Number of elements = 10947
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6395
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
ok
test_setInput (test_aflr3.TestAFLR3.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr3.TestAFLR3.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5047
Number of elements = 27987
Number of triangles = 3464
Number of quadrilatarals = 0
Number of tetrahedrals = 24523
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_torus (test_aflr3.TestAFLR3.test_torus) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6442
Number of elements = 36024
Number of triangles = 4052
Number of quadrilatarals = 0
Number of tetrahedrals = 31972
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_transp (test_aflr3.TestAFLR3.test_transp) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 59849
Number of elements = 349298
Number of triangles = 12928
Number of quadrilatarals = 0
Number of tetrahedrals = 336370
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 59428
Number of elements = 346223
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 333795
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 59849
Number of elements = 348798
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 336370
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_MultiBody_quad (test_aflr4.TestAFLR4.test_MultiBody_quad) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
ok
test_SingleBody_output (test_aflr4.TestAFLR4.test_SingleBody_output) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - trailingEdge
Done getting mesh sizing parameters
ok
test_all (test_aflr4.TestAFLR4.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
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:62030)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
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:62030)
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:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
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:62030)
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ok
test_reenter (test_aflr4.TestAFLR4.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
ok
test_setInput (test_aflr4.TestAFLR4.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr4.TestAFLR4.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_torus (test_aflr4.TestAFLR4.test_torus) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_Aeroelastic (test_astros.TestAstros.test_Aeroelastic) ... skipped 'No astros.exe executable'
test_Plate (test_astros.TestAstros.test_Plate) ... skipped 'No astros.exe executable'
test_MassProp_Units (test_avl.TestAVL.test_MassProp_Units) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_MassProp_noUnits (test_avl.TestAVL.test_MassProp_noUnits) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_alpha_custom_increment (test_avl.TestAVL.test_alpha_custom_increment) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_geom_change (test_avl.TestAVL.test_geom_change) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
ok
test_numSpan (test_avl.TestAVL.test_numSpan) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
ok
test_phase (test_avl.TestAVL.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_wing_Vtail (test_avl.TestAVL.test_wing_Vtail) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - VTail1
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - VTail2
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - VTail1 (ID = 0)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - VTail2 (ID = 1)
Section 1 of 2 (ID = 0)
Section 2 of 2 (ID = 1)
Writing surface - Wing (ID = 2)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
ok
test_wing_tail (test_avl.TestAVL.test_wing_tail) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
VLM surface name - hTail
VLM surface name - vTail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing surface - hTail (ID = 1)
Section 1 of 3 (ID = 2)
Control surface 1 of 1
Section 2 of 3 (ID = 1)
Control surface 1 of 1
Section 3 of 3 (ID = 0)
Control surface 1 of 1
Writing surface - vTail (ID = 2)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
ok
test_wing_tail_control (test_avl.TestAVL.test_wing_tail_control) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice control surface data
VLM control surface name - Elevator
VLM control surface name - LeftAileron
VLM control surface name - RightAileron
VLM control surface name - Rudder
Done getting vortex lattice control surface data
Getting vortex lattice surface data
VLM surface name - Wing
VLM surface name - hTail
VLM surface name - vTail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing surface - hTail (ID = 1)
Section 1 of 3 (ID = 2)
Control surface 1 of 1
Section 2 of 3 (ID = 1)
Control surface 1 of 1
Section 3 of 3 (ID = 0)
Control surface 1 of 1
Writing surface - vTail (ID = 2)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
ok
test_TargetCL (test_cart3d.TestCart3D.test_TargetCL) ... skipped 'No flowCart executable'
test_outputs (test_cart3d.TestCart3D.test_outputs) ... skipped 'No flowCart executable'
test_reenter (test_cart3d.TestCart3D.test_reenter) ... skipped 'No flowCart executable'
test_sensitivity_AnalysisIn (test_cart3d.TestCart3D.test_sensitivity_AnalysisIn) ... skipped 'No flowCart executable'
test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... skipped 'No flowCart executable'
test_Output_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:62030)
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
7F5CBD582740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7F5CBD582740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7F5C9E4E3700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7F5C9E4E3700 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
7F5C9F4E5700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7F5C9F4E5700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7F5C9ECE4700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7F5C9ECE4700 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
7F5C9ECE4700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7F5C9ECE4700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7F5CBD582740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7F5CBD582740 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
7F5CBD582740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7F5CBD582740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7F5C9F4E5700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7F5C9F4E5700 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:62030)
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:62030)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
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:62030)
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:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
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:62030)
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:62030)
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:62030)
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:62030)
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: 0.151997
Creating surface mesh ...
Surface mesh seconds: 0.034887
Recovering boundaries...
Boundary recovery seconds: 0.143089
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.063902
Recovering Delaunayness...
Delaunay recovery seconds: 0.074543
Refining mesh...
18827 insertions, added 13420 points, 721721 tetrahedra in queue.
6269 insertions, added 2485 points, 625204 tetrahedra in queue.
8356 insertions, added 2101 points, 168215 tetrahedra in queue.
Refinement seconds: 2.98539
Smoothing vertices...
Mesh smoothing seconds: 2.87744
Improving mesh...
Mesh improvement seconds: 0.058237
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.017358
Total running seconds: 6.40753
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: 0.150372
Creating surface mesh ...
Surface mesh seconds: 0.036226
Recovering boundaries...
Boundary recovery seconds: 0.164632
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.07198
Recovering Delaunayness...
Delaunay recovery seconds: 0.075211
Refining mesh...
18827 insertions, added 13420 points, 721721 tetrahedra in queue.
6269 insertions, added 2485 points, 625204 tetrahedra in queue.
8356 insertions, added 2101 points, 168215 tetrahedra in queue.
Refinement seconds: 2.96138
Smoothing vertices...
Mesh smoothing seconds: 2.87039
Improving mesh...
Mesh improvement seconds: 0.089834
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.031922
Total running seconds: 6.45259
Statistics:
Input points: 14124
Input facets: 28236
Input segments: 42354
Input holes: 2
Input regions: 0
Mesh points: 33059
Mesh tetrahedra: 159851
Mesh faces: 333820
Mesh faces on exterior boundary: 28236
Mesh faces on input facets: 28236
Mesh edges on input segments: 42354
Steiner points inside domain: 18935
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM4/fun3d.nml .....
Appending namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
ok
test_cythonNMLError (test_fun3d.TestFUN3D.test_cythonNMLError) ... ok
test_cythonNMLReentrance (test_fun3d.TestFUN3D.test_cythonNMLReentrance) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml not found!
Creating namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml .....
Appending namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
ok
test_invalidBoundary (test_fun3d.TestFUN3D.test_invalidBoundary) ... Getting CFD boundary conditions
Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_fun3d.TestFUN3D.test_invalidBoundaryName) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - X
ok
test_journal (test_fun3d.TestFUN3D.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 5043, elements - 10074
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 5043, elements - 10074
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
ok
test_moving_body (test_fun3d.TestFUN3D.test_moving_body) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Writing moving_body.input
ok
test_overwriteNML (test_fun3d.TestFUN3D.test_overwriteNML) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_phase (test_fun3d.TestFUN3D.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 14124, elements - 28236
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_reenter (test_fun3d.TestFUN3D.test_reenter) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
ok
test_symmetry (test_fun3d.TestFUN3D.test_symmetry) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_box1 (test_masstran.TestMasstran.test_box1) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_box2 (test_masstran.TestMasstran.test_box2) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_box3 (test_masstran.TestMasstran.test_box3) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - box2
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
ok
test_journal (test_masstran.TestMasstran.test_journal) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
ok
test_plate (test_masstran.TestMasstran.test_plate) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_plate_point (test_masstran.TestMasstran.test_plate_point) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
ok
test_Cheby_Modes (test_mses.TestMSES_Kulfan.test_Cheby_Modes) ...
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - alowervar
Design Variable name - auppervar
Design Variable name - classvar
Design Variable name - ztailvar
Done getting CFD design variables
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_Kulfan.test_Cheby_Modes_Symmetric) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - avar
Done getting CFD design variables
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_allInputs (test_mses.TestMSES_Kulfan.test_allInputs) ... ok
test_execute (test_mses.TestMSES_Kulfan.test_execute) ... ok
test_sensitivity_AnalysisIn (test_mses.TestMSES_Kulfan.test_sensitivity_AnalysisIn) ... ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_NACA.test_Cheby_Modes_Symmetric) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
ok
test_geom_sensitivity_CL (test_mses.TestMSES_NACA.test_geom_sensitivity_CL) ...
Getting CFD design variables.......
Number of design variables - 2
Design Variable name - camber
Design Variable name - thick
Done getting CFD design variables
ok
test_journal (test_mses.TestMSES_NACA.test_journal) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
ok
test_MultiBody (test_pointwise.TestPointwise.test_MultiBody) ... skipped 'No pointwise executable'
test_SingleBody (test_pointwise.TestPointwise.test_SingleBody) ... skipped 'No pointwise executable'
test_all (test_pointwise.TestPointwise.test_all) ... skipped 'No pointwise executable'
test_box (test_pointwise.TestPointwise.test_box) ... skipped 'No pointwise executable'
test_bullet (test_pointwise.TestPointwise.test_bullet) ... skipped 'No pointwise executable'
test_cone (test_pointwise.TestPointwise.test_cone) ... skipped 'No pointwise executable'
test_cylinder (test_pointwise.TestPointwise.test_cylinder) ... skipped 'No pointwise executable'
test_executeError (test_pointwise.TestPointwise.test_executeError) ... skipped 'No pointwise executable'
test_reenter (test_pointwise.TestPointwise.test_reenter) ... skipped 'No pointwise executable'
test_sphere (test_pointwise.TestPointwise.test_sphere) ... skipped 'No pointwise executable'
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
test_Area_Mesh (test_refine.TestREFINE.test_Area_Mesh) ... skipped "No 'ref' executable"
test_all (test_refine.TestREFINE.test_all) ... skipped "No 'ref' executable"
test_box_volume (test_refine.TestREFINE.test_box_volume) ... skipped "No 'ref' executable"
test_boxhole (test_refine.TestREFINE.test_boxhole) ... skipped "No 'ref' executable"
test_cfdSingleBody (test_refine.TestREFINE.test_cfdSingleBody) ... skipped "No 'ref' executable"
test_fun3d (test_refine.TestREFINE.test_fun3d) ... skipped "No 'ref' executable"
test_inputs (test_refine.TestREFINE.test_inputs) ... skipped "No 'ref' executable"
test_phase (test_refine.TestREFINE.test_phase) ... skipped "No 'ref' executable"
test_sphere (test_refine.TestREFINE.test_sphere) ... skipped "No 'ref' executable"
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
test_inputs (test_su2.TestSU2.test_inputs) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
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 = 0.015 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 = 0.180 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 = 5.959 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 = 2.137 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 = 0.068 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 = 8.771 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 1.25
EGADS : OpenCASCADE Version 7.7.0
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 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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:62030)
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)
7F5C9F4E5700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7F5CBD582740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7F5CBD582740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
7F5C9F4E5700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, 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 144 tests in 488.732s
OK (skipped=26)
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/
+ make test TYPE=MINIMAL
(make -C cCAPS -f aeroelastic_SU2.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'avlTest' is up to date.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'awaveTest' is up to date.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'frictionTest' is up to date.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: Nothing to be done for 'fun3d'.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f hsm.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'hsm' is up to date.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'interferenceTest' is up to date.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'msesTest' is up to date.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f mystran.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'mystranTest' is up to date.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'pointwiseTest' is up to date.
make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/ESP_venv/bin/python
=================================================
Running.... MINIMAL PyTests
=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/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 0m0.865s
user 0m0.677s
sys 0m0.400s
+ 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/7.7/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/7.7/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 0m4.848s
user 0m4.723s
sys 0m0.316s
+ 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/7.7/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/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl = 0.37837910855492196
Cd = 0.007775858417210155
Cm = 0.005262636995812415
real 0m4.973s
user 0m4.804s
sys 0m0.368s
+ 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/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/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 0m0.424s
user 0m0.376s
sys 0m0.225s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'egadsTess_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ python -u egadsTess_PyTest.py -outLevel=0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Rib_Root_Point, index = 6
Name = Wing, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = LeadingEdge, index = 1
Name = TrailingEdge, index = 2
Getting mesh sizing parameters
Mesh sizing name - LeadingEdge
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 4)
Getting surface mesh for body 2 (of 4)
Getting surface mesh for body 3 (of 4)
Getting surface mesh for body 4 (of 4)
Body 1 (of 4)
Number of nodes = 3793
Number of elements = 4001
Number of triangle elements = 0
Number of quadrilateral elements = 4001
Body 2 (of 4)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes = 76
Number of elements = 55
Number of triangle elements = 0
Number of quadrilateral elements = 55
Body 4 (of 4)
Number of nodes = 100
Number of elements = 73
Number of triangle elements = 0
Number of quadrilateral elements = 73
----------------------------
Total number of nodes = 3970
Total number of elements = 4129
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
real 0m7.215s
user 0m13.012s
sys 0m0.682s
+ 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/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/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 = 0.002 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 = 0.030 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 = 0.012 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 0m0.615s
user 0m0.678s
sys 0m0.281s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr4_and_aflr3_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_aflr3_PyTest.py test;
+ python -u aflr4_and_aflr3_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Wing1
Mesh sizing name - Wing2
Done getting mesh sizing parameters
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 04/23/24 @ 12:17PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR4 : Compile Date 04/23/24 @ 12:17PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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 0m15.144s
user 0m14.879s
sys 0m0.396s
+ 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/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/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: 0.024999
Creating surface mesh ...
Surface mesh seconds: 0.00765
Recovering boundaries...
Boundary recovery seconds: 0.071559
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.01704
Suppressing Steiner points ...
Steiner suppression seconds: 8.9e-05
Recovering Delaunayness...
Delaunay recovery seconds: 0.032599
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: 0.746267
Smoothing vertices...
Mesh smoothing seconds: 0.601176
Improving mesh...
Mesh improvement seconds: 0.014724
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.003876
Total running seconds: 1.52026
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 0m2.970s
user 0m3.241s
sys 0m0.320s
+ 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/7.7/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/7.7/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 = 0.005 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 = 0.088 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 = 0.021 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| 1.3301e-01| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.2935e-01| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.2580e-01| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.2055e-01| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.1578e-01| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.1313e-01| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.1113e-01| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.0962e-01| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.0842e-01| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.0750e-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 0m2.543s
user 0m2.409s
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/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/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 0m3.904s
user 0m6.259s
sys 0m1.087s
+ 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/7.7/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/7.7/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 0m0.971s
user 0m0.919s
sys 0m0.280s
+ 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/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
../corsairlite/qp.py test;
+ python -u ../corsairlite/qp.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/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 0m2.425s
user 0m2.564s
sys 0m0.483s
+ 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/7.7/LINUX64
+ mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/test/plugs
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/test/plugs
+ find /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/Plugs -name 'plugs0*.csm'
+ sort -f
find: ‘/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64/JenkinsESP/data/plugs/plugsFailure.txt
+ cp /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/JenkinsESP/data/plugs/plugsIgnore.txt .
+ set +x
Testing CSM files:
total 31M
-rw-rw-r--. 1 jenkins jenkins 1.3M May 30 12:23 ASTRO.D01
-rw-rw-r--. 1 jenkins jenkins 316K May 30 12:23 ASTRO.IDX
-rwxrwxr-x. 1 jenkins jenkins 1.1M May 30 12:23 avl
-rwxrwxr-x. 1 jenkins jenkins 41K May 30 12:21 egads2cart
-rwxrwxr-x. 1 jenkins jenkins 140K May 30 12:24 egads2cgt
-rwxrwxr-x. 1 jenkins jenkins 54K May 30 12:23 friction
-rwxrwxr-x. 1 jenkins jenkins 8.2M May 30 12:23 mastros.exe
-rwxrwxr-x. 1 jenkins jenkins 727K May 30 12:23 mses
-rwxrwxr-x. 1 jenkins jenkins 536K May 30 12:23 mset
-rwxrwxr-x. 1 jenkins jenkins 51K May 30 12:23 phaseUtil
-rw-rw-r--. 1 jenkins jenkins 1.6K May 30 12:26 pod.egads
-rw-rw-r--. 1 jenkins jenkins 0 May 30 12:26 port7681.jrnl
-rwxrwxr-x. 1 jenkins jenkins 451K May 30 12:23 pplot
-rwxrwxr-x. 1 jenkins jenkins 405K May 30 12:23 pxplot
-rwxrwxr-x. 1 jenkins jenkins 143K May 30 12:22 sensCSM
-rwxrwxr-x. 1 jenkins jenkins 624K May 30 12:22 serveCSM
-rwxrwxr-x. 1 jenkins jenkins 537K May 30 12:22 serveESP
-rwxrwxr-x. 1 jenkins jenkins 719K May 30 12:23 Slugs
-rwxrwxr-x. 1 jenkins jenkins 210K May 30 12:23 TestFit
-rwxrwxr-x. 1 jenkins jenkins 78K May 30 12:21 vCurvature
-rwxrwxr-x. 1 jenkins jenkins 50K May 30 12:21 vGeom
-rwxrwxr-x. 1 jenkins jenkins 80K May 30 12:21 vTess
-rwxrwxr-x. 1 jenkins jenkins 14M May 30 12:21 vTesstatic
-rw-rw-r--. 1 jenkins jenkins 195K May 30 12:25 wingMultiModel.bdf
-rwxrwxr-x. 1 jenkins jenkins 1.1M May 30 12:23 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/7.7/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/7.7/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.7/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/7.7/LINUX64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.7/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=7.7,ESP_ARCH=LINUX64,buildnode=reynolds-centOS8 #720'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS