Started by upstream project "ESP_Beta" build number 723
originally caused by:
Started by remote host 18.18.33.14
Running as SYSTEM
[EnvInject] - Loading node environment variables.
Building remotely on reynolds-centOS7 in workspace /home/jenkins/workspace/ESP_Beta/7.8/LINUX64
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] Done
Checking out a fresh workspace because there's no workspace at /home/jenkins/workspace/ESP_Beta/7.8/LINUX64
Cleaning local Directory .
Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-06-18T21:16:10.397 -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 2506
Checking out a fresh workspace because /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP doesn't exist
Cleaning local Directory JenkinsESP
Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-06-18T21:16:10.397 -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 867
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-centOS7] is in [[macys, macys_VM, reynolds, reynolds-centOS7, reynolds-centOS8, reynolds-ubuntu18]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[LINUX64] $ /bin/bash -ex /tmp/jenkins3733143150509764191.sh
+ bash -ex /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/ESP_Beta.sh
+ source /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.8
++ OCCTREF=7.8
++ AFLR_VERSION=11.5.14
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.38.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ reynolds-centOS7 == \r\e\y\n\o\l\d\s ]]
++ [[ LINUX64 == *\.\i\f\o\r\t ]]
++ '[' -f /opt/intel/oneapi/setvars.sh ']'
++ '[' -f /home/jenkins/.bashrc ']'
++ source /home/jenkins/.bashrc
+++ '[' -f /etc/bashrc ']'
+++ . /etc/bashrc
++++ '[' '' ']'
++++ shopt -q login_shell
++++ '[' 1001 -gt 199 ']'
+++++ /usr/bin/id -gn
+++++ /usr/bin/id -un
++++ '[' jenkins = jenkins ']'
++++ umask 002
++++ SHELL=/bin/bash
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/256term.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/256term.sh
+++++ local256=
+++++ '[' -n '' ']'
+++++ '[' -n '' ']'
+++++ unset local256
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/abrt-console-notification.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/abrt-console-notification.sh
+++++ tty -s
+++++ return 0
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/bash_completion.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/bash_completion.sh
+++++ '[' -z '4.2.46(2)-release' -o -z '' -o -n '' ']'
+++++ return
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/colorgrep.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/colorgrep.sh
+++++ /usr/libexec/grepconf.sh -c
+++++ alias 'grep=grep --color=auto'
+++++ alias 'egrep=egrep --color=auto'
+++++ alias 'fgrep=fgrep --color=auto'
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/colorls.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/colorls.sh
+++++ '[' '!' -t 0 ']'
+++++ return
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/flatpak.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/flatpak.sh
+++++ '[' /exports/share:/var/lib/flatpak/exports/share:/usr/local/share:/usr/share = /home/jenkins/.local/share/flatpak/exports/share:/var/lib/flatpak/exports/share:/usr/local/share:/usr/share ']'
+++++ export XDG_DATA_DIRS
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/lang.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/lang.sh
+++++ sourced=0
+++++ '[' -n en_US.UTF-8 ']'
+++++ saved_lang=en_US.UTF-8
+++++ '[' -f /home/jenkins/.i18n ']'
+++++ LANG=en_US.UTF-8
+++++ unset saved_lang
+++++ '[' 0 = 1 ']'
+++++ unset sourced
+++++ unset langfile
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/less.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/less.sh
+++++ '[' -x /usr/bin/lesspipe.sh ']'
+++++ export 'LESSOPEN=||/usr/bin/lesspipe.sh %s'
+++++ LESSOPEN='||/usr/bin/lesspipe.sh %s'
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/PackageKit.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/PackageKit.sh
+++++ [[ -n '' ]]
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/vim.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/vim.sh
+++++ '[' -n '4.2.46(2)-release' -o -n '' -o -n '' ']'
+++++ '[' -x /usr/bin/id ']'
++++++ /usr/bin/id -u
+++++ ID=1001
+++++ '[' -n 1001 -a 1001 -le 200 ']'
+++++ alias vi
+++++ alias vi=vim
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/vte.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/vte.sh
+++++ '[' -n '4.2.46(2)-release' -o -n '' ']'
+++++ [[ ehxB == *i* ]]
+++++ return 0
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/which2.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/which2.sh
+++++ alias 'which=alias | /usr/bin/which --tty-only --read-alias --show-dot --show-tilde'
++++ unset i
++++ unset -f pathmunge
++ export CAPS_OUTLEVEL=0
++ CAPS_OUTLEVEL=0
++ [[ LINUX64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64
++ ESP_BLOC=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64
++ export ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64
++ ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64
++ export JULIA_DEPOT_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/julia
++ JULIA_DEPOT_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.8 != '' ]]
++ [[ '' != '' ]]
++ [[ reynolds-centOS7 == *\r\e\y\n\o\l\d\s* ]]
++ [[ '' != '' ]]
++ [[ -d /home/jenkins/util/ESP/Python/ESP_Python-3.11.9 ]]
++ export PYTHONHOME=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9
++ PYTHONHOME=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9
++ export PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ export LD_LIBRARY_PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ LD_LIBRARY_PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ export EMPnumProc=4
++ EMPnumProc=4
++ export OMP_NUM_THREADS=4
++ OMP_NUM_THREADS=4
++ '[' '!' -z '' ']'
+++ ls -d /home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export CASARCH=.
++ CASARCH=.
++ export LD_LIBRARY_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ LD_LIBRARY_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ export ESP_EXTERN_LIBS=/home/jenkins/util/ESP/ExternLibs
++ ESP_EXTERN_LIBS=/home/jenkins/util/ESP/ExternLibs
++ export AFLR=/home/jenkins/util/AFLR/aflr_lib_11.5.14
++ AFLR=/home/jenkins/util/AFLR/aflr_lib_11.5.14
++ export AFLR_ARCH=Linux-x86-64
++ AFLR_ARCH=Linux-x86-64
++ export PATH=/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ export CART3D=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16
++ CART3D=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16
++ export CART3D_ARCH=X86_64_ICC
++ CART3D_ARCH=X86_64_ICC
++ export PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ export PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ export PATH=/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ export PATH=/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ export MYSTRAN_directory=/home/jenkins/util/mystran/MYSTRAN/Binaries
++ MYSTRAN_directory=/home/jenkins/util/mystran/MYSTRAN/Binaries
++ export PATH=/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ export PATH=/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ export CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/aim/pointwise/glyph
++ export PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ [[ reynolds-centOS7 == \r\e\y\n\o\l\d\s ]]
++ export SU2_HOME=/home/jenkins/util/SU2/SU2-v8.0.0
++ SU2_HOME=/home/jenkins/util/SU2/SU2-v8.0.0
++ export SU2_RUN=/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ SU2_RUN=/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ export PATH=/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ '[' -d /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16 ']'
++ export PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ [[ reynolds-centOS7 == \m\a\c\y\s* ]]
++ [[ reynolds-centOS7 == \v\i\g\g\e\n ]]
+++ python-config --includes
++ export 'PYTHONINC=. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
++ PYTHONINC='. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
+++ python-config --help
++ [[ Usage: /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python-config --prefix|--exec-prefix|--includes|--libs|--cflags|--ldflags|--extension-suffix|--help|--abiflags|--configdir|--embed == *\e\m\b\e\d* ]]
+++ python-config --ldflags --embed
++ export 'PYTHONLIB= -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lpthread -ldl -lutil -lm '
++ PYTHONLIB=' -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lpthread -ldl -lutil -lm '
++ [[ reynolds-centOS7 == \m\a\c\y\s ]]
++ [[ reynolds-centOS7 == \v\i\g\g\e\n ]]
++ export PYTHONUNBUFFERED=true
++ PYTHONUNBUFFERED=true
++ export PYTHONFAULTHANDLER=true
++ PYTHONFAULTHANDLER=true
++ python --version
Python 3.11.9
++ [[ LINUX64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export CSMDATA=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/data
++ CSMDATA=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/data
+ virtualenv /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv
created virtual environment CPython3.11.9.final.0-64 in 417ms
creator CPython3Posix(dest=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv, clear=False, no_vcs_ignore=False, global=False)
seeder FromAppData(download=False, pip=bundle, setuptools=bundle, wheel=bundle, via=copy, app_data_dir=/home/jenkins/.local/share/virtualenv)
added seed packages: pip==24.0, setuptools==70.0.0, wheel==0.43.0
activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator
+ . /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/activate
++ '[' /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/activate = /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/ESP_Beta.sh ']'
++ deactivate nondestructive
++ unset -f pydoc
++ '[' -z '' ']'
++ '[' -z '' ']'
++ hash -r
++ '[' -z '' ']'
++ unset VIRTUAL_ENV
++ unset VIRTUAL_ENV_PROMPT
++ '[' '!' nondestructive = nondestructive ']'
++ VIRTUAL_ENV=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv
++ '[' linux-gnu = cygwin ']'
++ '[' linux-gnu = msys ']'
++ export VIRTUAL_ENV
++ _OLD_VIRTUAL_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH
++ '[' x '!=' x ']'
+++ basename /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv
++ VIRTUAL_ENV_PROMPT=ESP_venv
++ export VIRTUAL_ENV_PROMPT
++ '[' -z _ ']'
++ _OLD_VIRTUAL_PYTHONHOME=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9
++ unset PYTHONHOME
++ '[' -z '' ']'
++ _OLD_VIRTUAL_PS1=
++ PS1='(ESP_venv) '
++ export PS1
++ alias pydoc
++ true
++ hash -r
+ pip_install pip
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade pip
Requirement already satisfied: pip in ./ESP_venv/lib/python3.11/site-packages (24.0)
+ pip_install f90nml
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade f90nml
Collecting f90nml
Using cached f90nml-1.4.4-py2.py3-none-any.whl.metadata (6.0 kB)
Using cached f90nml-1.4.4-py2.py3-none-any.whl (32 kB)
Installing collected packages: f90nml
Successfully installed f90nml-1.4.4
+ pip_install numpy
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade numpy
Collecting numpy
Using cached numpy-2.0.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (60 kB)
Using cached numpy-2.0.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (19.3 MB)
Installing collected packages: numpy
Successfully installed numpy-2.0.0
+ pip_install openmdao
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade openmdao
Collecting openmdao
Using cached openmdao-3.33.0-py3-none-any.whl
Collecting networkx>=2.0 (from openmdao)
Using cached networkx-3.3-py3-none-any.whl.metadata (5.1 kB)
Collecting numpy<2 (from openmdao)
Using cached numpy-1.26.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (61 kB)
Collecting packaging (from openmdao)
Using cached packaging-24.1-py3-none-any.whl.metadata (3.2 kB)
Collecting requests (from openmdao)
Using cached requests-2.32.3-py3-none-any.whl.metadata (4.6 kB)
Collecting scipy (from openmdao)
Using cached scipy-1.13.1-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 urllib3-2.2.2-py3-none-any.whl.metadata (6.4 kB)
Collecting certifi>=2017.4.17 (from requests->openmdao)
Using cached certifi-2024.6.2-py3-none-any.whl.metadata (2.2 kB)
Using cached networkx-3.3-py3-none-any.whl (1.7 MB)
Using cached numpy-1.26.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (18.3 MB)
Using cached packaging-24.1-py3-none-any.whl (53 kB)
Using cached requests-2.32.3-py3-none-any.whl (64 kB)
Using cached scipy-1.13.1-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (38.6 MB)
Using cached certifi-2024.6.2-py3-none-any.whl (164 kB)
Using cached charset_normalizer-3.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (140 kB)
Using cached idna-3.7-py3-none-any.whl (66 kB)
Using cached urllib3-2.2.2-py3-none-any.whl (121 kB)
Installing collected packages: urllib3, packaging, numpy, networkx, idna, charset-normalizer, certifi, scipy, requests, openmdao
Attempting uninstall: numpy
Found existing installation: numpy 2.0.0
Uninstalling numpy-2.0.0:
Successfully uninstalled numpy-2.0.0
Successfully installed certifi-2024.6.2 charset-normalizer-3.3.2 idna-3.7 networkx-3.3 numpy-1.26.4 openmdao-3.33.0 packaging-24.1 requests-2.32.3 scipy-1.13.1 urllib3-2.2.2
+ [[ reynolds-centOS7 == *\v\i\g\g\e\n* ]]
+ pip_install cvxopt
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade cvxopt
Collecting cvxopt
Using cached cvxopt-1.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (1.3 kB)
Using cached cvxopt-1.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (13.6 MB)
Installing collected packages: cvxopt
Successfully installed cvxopt-1.3.2
+ pip_install dill
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade dill
Collecting dill
Using cached dill-0.3.8-py3-none-any.whl.metadata (10 kB)
Using cached dill-0.3.8-py3-none-any.whl (116 kB)
Installing collected packages: dill
Successfully installed dill-0.3.8
+ pip_install packaging
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade packaging
Requirement already satisfied: packaging in ./ESP_venv/lib/python3.11/site-packages (24.1)
+ pip_install matplotlib
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade matplotlib
Collecting matplotlib
Using cached matplotlib-3.9.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (11 kB)
Collecting contourpy>=1.0.1 (from matplotlib)
Using cached contourpy-1.2.1-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (5.8 kB)
Collecting cycler>=0.10 (from matplotlib)
Using cached cycler-0.12.1-py3-none-any.whl.metadata (3.8 kB)
Collecting fonttools>=4.22.0 (from matplotlib)
Using cached fonttools-4.53.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (162 kB)
Collecting kiwisolver>=1.3.1 (from matplotlib)
Using cached kiwisolver-1.4.5-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (6.4 kB)
Requirement already satisfied: numpy>=1.23 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (1.26.4)
Requirement already satisfied: packaging>=20.0 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (24.1)
Collecting pillow>=8 (from matplotlib)
Using cached pillow-10.3.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (9.2 kB)
Collecting pyparsing>=2.3.1 (from matplotlib)
Using cached pyparsing-3.1.2-py3-none-any.whl.metadata (5.1 kB)
Collecting python-dateutil>=2.7 (from matplotlib)
Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl.metadata (8.4 kB)
Collecting six>=1.5 (from python-dateutil>=2.7->matplotlib)
Using cached six-1.16.0-py2.py3-none-any.whl.metadata (1.8 kB)
Using cached matplotlib-3.9.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (8.3 MB)
Using cached contourpy-1.2.1-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (306 kB)
Using cached cycler-0.12.1-py3-none-any.whl (8.3 kB)
Using cached fonttools-4.53.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (4.9 MB)
Using cached kiwisolver-1.4.5-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (1.4 MB)
Using cached pillow-10.3.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (4.4 MB)
Using cached pyparsing-3.1.2-py3-none-any.whl (103 kB)
Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl (229 kB)
Using cached six-1.16.0-py2.py3-none-any.whl (11 kB)
Installing collected packages: six, pyparsing, pillow, kiwisolver, fonttools, cycler, contourpy, python-dateutil, matplotlib
Successfully installed contourpy-1.2.1 cycler-0.12.1 fonttools-4.53.0 kiwisolver-1.4.5 matplotlib-3.9.0 pillow-10.3.0 pyparsing-3.1.2 python-dateutil-2.9.0.post0 six-1.16.0
+ pip_install scipy
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade scipy
Requirement already satisfied: scipy in ./ESP_venv/lib/python3.11/site-packages (1.13.1)
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
--2024-06-18 21:16:57-- 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: 272159479 (260M) [application/x-gzip]
Saving to: ‘ESPbeta.tgz’
0K .......... .......... .......... .......... .......... 0% 5.66M 46s
50K .......... .......... .......... .......... .......... 0% 12.2M 34s
100K .......... .......... .......... .......... .......... 0% 37.9M 25s
150K .......... .......... .......... .......... .......... 0% 5.19M 31s
200K .......... .......... .......... .......... .......... 0% 64.3M 26s
250K .......... .......... .......... .......... .......... 0% 90.1M 22s
300K .......... .......... .......... .......... .......... 0% 138M 19s
350K .......... .......... .......... .......... .......... 0% 12.4M 19s
400K .......... .......... .......... .......... .......... 0% 190M 17s
450K .......... .......... .......... .......... .......... 0% 25.9M 16s
500K .......... .......... .......... .......... .......... 0% 129M 15s
550K .......... .......... .......... .......... .......... 0% 9.86M 16s
600K .......... .......... .......... .......... .......... 0% 74.6M 15s
650K .......... .......... .......... .......... .......... 0% 167M 14s
700K .......... .......... .......... .......... .......... 0% 33.6M 14s
750K .......... .......... .......... .......... .......... 0% 35.5M 13s
800K .......... .......... .......... .......... .......... 0% 13.5M 14s
850K .......... .......... .......... .......... .......... 0% 24.8M 13s
900K .......... .......... .......... .......... .......... 0% 16.4M 14s
950K .......... .......... .......... .......... .......... 0% 23.1M 13s
1000K .......... .......... .......... .......... .......... 0% 6.58M 15s
1050K .......... .......... .......... .......... .......... 0% 64.2M 14s
1100K .......... .......... .......... .......... .......... 0% 148M 14s
1150K .......... .......... .......... .......... .......... 0% 17.2M 14s
1200K .......... .......... .......... .......... .......... 0% 18.8M 14s
1250K .......... .......... .......... .......... .......... 0% 11.5M 14s
1300K .......... .......... .......... .......... .......... 0% 18.1M 14s
1350K .......... .......... .......... .......... .......... 0% 11.8M 14s
1400K .......... .......... .......... .......... .......... 0% 16.4M 14s
1450K .......... .......... .......... .......... .......... 0% 11.5M 15s
1500K .......... .......... .......... .......... .......... 0% 16.5M 15s
1550K .......... .......... .......... .......... .......... 0% 13.4M 15s
1600K .......... .......... .......... .......... .......... 0% 14.9M 15s
1650K .......... .......... .......... .......... .......... 0% 14.9M 15s
1700K .......... .......... .......... .......... .......... 0% 13.1M 15s
1750K .......... .......... .......... .......... .......... 0% 14.7M 15s
1800K .......... .......... .......... .......... .......... 0% 15.0M 15s
1850K .......... .......... .......... .......... .......... 0% 11.0M 15s
1900K .......... .......... .......... .......... .......... 0% 14.0M 15s
1950K .......... .......... .......... .......... .......... 0% 11.2M 16s
2000K .......... .......... .......... .......... .......... 0% 20.6M 16s
2050K .......... .......... .......... .......... .......... 0% 20.1M 16s
2100K .......... .......... .......... .......... .......... 0% 12.8M 16s
2150K .......... .......... .......... .......... .......... 0% 16.9M 16s
2200K .......... .......... .......... .......... .......... 0% 11.9M 16s
2250K .......... .......... .......... .......... .......... 0% 25.8M 16s
2300K .......... .......... .......... .......... .......... 0% 14.3M 16s
2350K .......... .......... .......... .......... .......... 0% 16.7M 16s
2400K .......... .......... .......... .......... .......... 0% 23.6M 16s
2450K .......... .......... .......... .......... .......... 0% 13.2M 16s
2500K .......... .......... .......... .......... .......... 0% 15.1M 16s
2550K .......... .......... .......... .......... .......... 0% 18.3M 16s
2600K .......... .......... .......... .......... .......... 0% 23.4M 16s
2650K .......... .......... .......... .......... .......... 1% 12.4M 16s
2700K .......... .......... .......... .......... .......... 1% 17.3M 16s
2750K .......... .......... .......... .......... .......... 1% 24.3M 16s
2800K .......... .......... .......... .......... .......... 1% 15.7M 16s
2850K .......... .......... .......... .......... .......... 1% 14.1M 16s
2900K .......... .......... .......... .......... .......... 1% 17.3M 16s
2950K .......... .......... .......... .......... .......... 1% 11.7M 16s
3000K .......... .......... .......... .......... .......... 1% 19.3M 16s
3050K .......... .......... .......... .......... .......... 1% 7.50M 16s
3100K .......... .......... .......... .......... .......... 1% 154M 16s
3150K .......... .......... .......... .......... .......... 1% 13.3M 16s
3200K .......... .......... .......... .......... .......... 1% 11.0M 16s
3250K .......... .......... .......... .......... .......... 1% 12.3M 16s
3300K .......... .......... .......... .......... .......... 1% 21.3M 16s
3350K .......... .......... .......... .......... .......... 1% 8.90M 16s
3400K .......... .......... .......... .......... .......... 1% 23.8M 16s
3450K .......... .......... .......... .......... .......... 1% 8.02M 16s
3500K .......... .......... .......... .......... .......... 1% 12.7M 16s
3550K .......... .......... .......... .......... .......... 1% 18.7M 16s
3600K .......... .......... .......... .......... .......... 1% 11.3M 16s
3650K .......... .......... .......... .......... .......... 1% 11.4M 16s
3700K .......... .......... .......... .......... .......... 1% 10.8M 16s
3750K .......... .......... .......... .......... .......... 1% 16.4M 16s
3800K .......... .......... .......... .......... .......... 1% 12.2M 17s
3850K .......... .......... .......... .......... .......... 1% 10.2M 17s
3900K .......... .......... .......... .......... .......... 1% 20.4M 17s
3950K .......... .......... .......... .......... .......... 1% 10.8M 17s
4000K .......... .......... .......... .......... .......... 1% 14.7M 17s
4050K .......... .......... .......... .......... .......... 1% 11.5M 17s
4100K .......... .......... .......... .......... .......... 1% 11.5M 17s
4150K .......... .......... .......... .......... .......... 1% 5.92M 17s
4200K .......... .......... .......... .......... .......... 1% 228M 17s
4250K .......... .......... .......... .......... .......... 1% 22.8M 17s
4300K .......... .......... .......... .......... .......... 1% 10.4M 17s
4350K .......... .......... .......... .......... .......... 1% 7.77M 17s
4400K .......... .......... .......... .......... .......... 1% 6.98M 17s
4450K .......... .......... .......... .......... .......... 1% 26.1M 17s
4500K .......... .......... .......... .......... .......... 1% 8.69M 17s
4550K .......... .......... .......... .......... .......... 1% 8.08M 18s
4600K .......... .......... .......... .......... .......... 1% 7.38M 18s
4650K .......... .......... .......... .......... .......... 1% 8.14M 18s
4700K .......... .......... .......... .......... .......... 1% 6.53M 18s
4750K .......... .......... .......... .......... .......... 1% 11.3M 18s
4800K .......... .......... .......... .......... .......... 1% 10.7M 18s
4850K .......... .......... .......... .......... .......... 1% 6.20M 18s
4900K .......... .......... .......... .......... .......... 1% 10.4M 18s
4950K .......... .......... .......... .......... .......... 1% 9.15M 19s
5000K .......... .......... .......... .......... .......... 1% 10.6M 19s
5050K .......... .......... .......... .......... .......... 1% 8.22M 19s
5100K .......... .......... .......... .......... .......... 1% 6.69M 19s
5150K .......... .......... .......... .......... .......... 1% 9.55M 19s
5200K .......... .......... .......... .......... .......... 1% 11.4M 19s
5250K .......... .......... .......... .......... .......... 1% 12.8M 19s
5300K .......... .......... .......... .......... .......... 2% 9.63M 19s
5350K .......... .......... .......... .......... .......... 2% 11.4M 19s
5400K .......... .......... .......... .......... .......... 2% 10.1M 19s
5450K .......... .......... .......... .......... .......... 2% 7.53M 19s
5500K .......... .......... .......... .......... .......... 2% 10.9M 19s
5550K .......... .......... .......... .......... .......... 2% 11.2M 19s
5600K .......... .......... .......... .......... .......... 2% 11.5M 19s
5650K .......... .......... .......... .......... .......... 2% 11.5M 19s
5700K .......... .......... .......... .......... .......... 2% 9.91M 19s
5750K .......... .......... .......... .......... .......... 2% 13.0M 19s
5800K .......... .......... .......... .......... .......... 2% 12.1M 19s
5850K .......... .......... .......... .......... .......... 2% 11.8M 19s
5900K .......... .......... .......... .......... .......... 2% 11.8M 19s
5950K .......... .......... .......... .......... .......... 2% 11.5M 19s
6000K .......... .......... .......... .......... .......... 2% 11.4M 19s
6050K .......... .......... .......... .......... .......... 2% 12.6M 19s
6100K .......... .......... .......... .......... .......... 2% 11.1M 20s
6150K .......... .......... .......... .......... .......... 2% 57.1M 19s
6200K .......... .......... .......... .......... .......... 2% 11.2M 19s
6250K .......... .......... .......... .......... .......... 2% 11.3M 19s
6300K .......... .......... .......... .......... .......... 2% 11.3M 19s
6350K .......... .......... .......... .......... .......... 2% 8.89M 20s
6400K .......... .......... .......... .......... .......... 2% 16.5M 19s
6450K .......... .......... .......... .......... .......... 2% 11.4M 20s
6500K .......... .......... .......... .......... .......... 2% 14.1M 19s
6550K .......... .......... .......... .......... .......... 2% 27.4M 19s
6600K .......... .......... .......... .......... .......... 2% 13.0M 19s
6650K .......... .......... .......... .......... .......... 2% 11.5M 19s
6700K .......... .......... .......... .......... .......... 2% 11.7M 19s
6750K .......... .......... .......... .......... .......... 2% 18.1M 19s
6800K .......... .......... .......... .......... .......... 2% 17.8M 19s
6850K .......... .......... .......... .......... .......... 2% 12.6M 19s
6900K .......... .......... .......... .......... .......... 2% 11.4M 19s
6950K .......... .......... .......... .......... .......... 2% 10.9M 19s
7000K .......... .......... .......... .......... .......... 2% 39.2M 19s
7050K .......... .......... .......... .......... .......... 2% 13.3M 19s
7100K .......... .......... .......... .......... .......... 2% 5.07M 19s
7150K .......... .......... .......... .......... .......... 2% 208M 19s
7200K .......... .......... .......... .......... .......... 2% 13.7M 19s
7250K .......... .......... .......... .......... .......... 2% 11.9M 19s
7300K .......... .......... .......... .......... .......... 2% 12.1M 19s
7350K .......... .......... .......... .......... .......... 2% 9.51M 19s
7400K .......... .......... .......... .......... .......... 2% 12.7M 19s
7450K .......... .......... .......... .......... .......... 2% 11.3M 19s
7500K .......... .......... .......... .......... .......... 2% 12.8M 19s
7550K .......... .......... .......... .......... .......... 2% 12.2M 19s
7600K .......... .......... .......... .......... .......... 2% 11.4M 19s
7650K .......... .......... .......... .......... .......... 2% 12.0M 19s
7700K .......... .......... .......... .......... .......... 2% 11.8M 19s
7750K .......... .......... .......... .......... .......... 2% 12.4M 19s
7800K .......... .......... .......... .......... .......... 2% 13.9M 19s
7850K .......... .......... .......... .......... .......... 2% 11.9M 19s
7900K .......... .......... .......... .......... .......... 2% 13.1M 19s
7950K .......... .......... .......... .......... .......... 3% 11.9M 19s
8000K .......... .......... .......... .......... .......... 3% 13.0M 19s
8050K .......... .......... .......... .......... .......... 3% 13.2M 19s
8100K .......... .......... .......... .......... .......... 3% 12.4M 19s
8150K .......... .......... .......... .......... .......... 3% 12.5M 19s
8200K .......... .......... .......... .......... .......... 3% 11.6M 19s
8250K .......... .......... .......... .......... .......... 3% 13.2M 19s
8300K .......... .......... .......... .......... .......... 3% 11.9M 19s
8350K .......... .......... .......... .......... .......... 3% 10.2M 19s
8400K .......... .......... .......... .......... .......... 3% 13.9M 19s
8450K .......... .......... .......... .......... .......... 3% 11.6M 19s
8500K .......... .......... .......... .......... .......... 3% 16.1M 19s
8550K .......... .......... .......... .......... .......... 3% 13.2M 19s
8600K .......... .......... .......... .......... .......... 3% 20.2M 19s
8650K .......... .......... .......... .......... .......... 3% 11.9M 19s
8700K .......... .......... .......... .......... .......... 3% 11.6M 19s
8750K .......... .......... .......... .......... .......... 3% 13.3M 19s
8800K .......... .......... .......... .......... .......... 3% 56.8M 19s
8850K .......... .......... .......... .......... .......... 3% 10.5M 19s
8900K .......... .......... .......... .......... .......... 3% 13.0M 19s
8950K .......... .......... .......... .......... .......... 3% 11.4M 19s
9000K .......... .......... .......... .......... .......... 3% 19.2M 19s
9050K .......... .......... .......... .......... .......... 3% 18.9M 19s
9100K .......... .......... .......... .......... .......... 3% 11.3M 19s
9150K .......... .......... .......... .......... .......... 3% 10.3M 19s
9200K .......... .......... .......... .......... .......... 3% 14.4M 19s
9250K .......... .......... .......... .......... .......... 3% 24.6M 19s
9300K .......... .......... .......... .......... .......... 3% 16.5M 19s
9350K .......... .......... .......... .......... .......... 3% 10.7M 19s
9400K .......... .......... .......... .......... .......... 3% 12.8M 19s
9450K .......... .......... .......... .......... .......... 3% 24.3M 19s
9500K .......... .......... .......... .......... .......... 3% 16.2M 19s
9550K .......... .......... .......... .......... .......... 3% 12.6M 19s
9600K .......... .......... .......... .......... .......... 3% 17.6M 19s
9650K .......... .......... .......... .......... .......... 3% 13.3M 19s
9700K .......... .......... .......... .......... .......... 3% 23.8M 19s
9750K .......... .......... .......... .......... .......... 3% 12.0M 19s
9800K .......... .......... .......... .......... .......... 3% 31.5M 19s
9850K .......... .......... .......... .......... .......... 3% 13.1M 19s
9900K .......... .......... .......... .......... .......... 3% 17.0M 19s
9950K .......... .......... .......... .......... .......... 3% 13.9M 19s
10000K .......... .......... .......... .......... .......... 3% 15.0M 19s
10050K .......... .......... .......... .......... .......... 3% 15.6M 19s
10100K .......... .......... .......... .......... .......... 3% 13.1M 19s
10150K .......... .......... .......... .......... .......... 3% 37.7M 19s
10200K .......... .......... .......... .......... .......... 3% 14.1M 19s
10250K .......... .......... .......... .......... .......... 3% 22.2M 19s
10300K .......... .......... .......... .......... .......... 3% 23.6M 19s
10350K .......... .......... .......... .......... .......... 3% 13.0M 19s
10400K .......... .......... .......... .......... .......... 3% 79.0M 19s
10450K .......... .......... .......... .......... .......... 3% 12.2M 19s
10500K .......... .......... .......... .......... .......... 3% 13.4M 19s
10550K .......... .......... .......... .......... .......... 3% 15.3M 19s
10600K .......... .......... .......... .......... .......... 4% 23.2M 19s
10650K .......... .......... .......... .......... .......... 4% 18.3M 19s
10700K .......... .......... .......... .......... .......... 4% 11.7M 19s
10750K .......... .......... .......... .......... .......... 4% 26.8M 19s
10800K .......... .......... .......... .......... .......... 4% 16.6M 19s
10850K .......... .......... .......... .......... .......... 4% 24.8M 19s
10900K .......... .......... .......... .......... .......... 4% 17.1M 19s
10950K .......... .......... .......... .......... .......... 4% 10.7M 19s
11000K .......... .......... .......... .......... .......... 4% 67.5M 18s
11050K .......... .......... .......... .......... .......... 4% 10.6M 18s
11100K .......... .......... .......... .......... .......... 4% 13.2M 18s
11150K .......... .......... .......... .......... .......... 4% 38.5M 18s
11200K .......... .......... .......... .......... .......... 4% 11.6M 18s
11250K .......... .......... .......... .......... .......... 4% 67.4M 18s
11300K .......... .......... .......... .......... .......... 4% 6.53M 18s
11350K .......... .......... .......... .......... .......... 4% 45.0M 18s
11400K .......... .......... .......... .......... .......... 4% 47.6M 18s
11450K .......... .......... .......... .......... .......... 4% 12.1M 18s
11500K .......... .......... .......... .......... .......... 4% 17.0M 18s
11550K .......... .......... .......... .......... .......... 4% 12.5M 18s
11600K .......... .......... .......... .......... .......... 4% 11.6M 18s
11650K .......... .......... .......... .......... .......... 4% 40.5M 18s
11700K .......... .......... .......... .......... .......... 4% 13.8M 18s
11750K .......... .......... .......... .......... .......... 4% 13.8M 18s
11800K .......... .......... .......... .......... .......... 4% 13.4M 18s
11850K .......... .......... .......... .......... .......... 4% 11.4M 18s
11900K .......... .......... .......... .......... .......... 4% 25.3M 18s
11950K .......... .......... .......... .......... .......... 4% 12.2M 18s
12000K .......... .......... .......... .......... .......... 4% 11.8M 18s
12050K .......... .......... .......... .......... .......... 4% 12.2M 18s
12100K .......... .......... .......... .......... .......... 4% 8.75M 18s
12150K .......... .......... .......... .......... .......... 4% 19.1M 18s
12200K .......... .......... .......... .......... .......... 4% 10.2M 18s
12250K .......... .......... .......... .......... .......... 4% 11.9M 18s
12300K .......... .......... .......... .......... .......... 4% 12.2M 18s
12350K .......... .......... .......... .......... .......... 4% 9.39M 18s
12400K .......... .......... .......... .......... .......... 4% 10.7M 18s
12450K .......... .......... .......... .......... .......... 4% 12.5M 18s
12500K .......... .......... .......... .......... .......... 4% 10.7M 18s
12550K .......... .......... .......... .......... .......... 4% 10.9M 18s
12600K .......... .......... .......... .......... .......... 4% 10.4M 18s
12650K .......... .......... .......... .......... .......... 4% 10.2M 18s
12700K .......... .......... .......... .......... .......... 4% 8.79M 18s
12750K .......... .......... .......... .......... .......... 4% 10.0M 18s
12800K .......... .......... .......... .......... .......... 4% 10.9M 18s
12850K .......... .......... .......... .......... .......... 4% 8.68M 19s
12900K .......... .......... .......... .......... .......... 4% 11.5M 19s
12950K .......... .......... .......... .......... .......... 4% 7.91M 19s
13000K .......... .......... .......... .......... .......... 4% 6.14M 19s
13050K .......... .......... .......... .......... .......... 4% 19.0M 19s
13100K .......... .......... .......... .......... .......... 4% 5.78M 19s
13150K .......... .......... .......... .......... .......... 4% 6.54M 19s
13200K .......... .......... .......... .......... .......... 4% 5.40M 19s
13250K .......... .......... .......... .......... .......... 5% 6.12M 19s
13300K .......... .......... .......... .......... .......... 5% 6.86M 19s
13350K .......... .......... .......... .......... .......... 5% 6.77M 19s
13400K .......... .......... .......... .......... .......... 5% 7.41M 19s
13450K .......... .......... .......... .......... .......... 5% 5.59M 19s
13500K .......... .......... .......... .......... .......... 5% 8.30M 19s
13550K .......... .......... .......... .......... .......... 5% 7.68M 19s
13600K .......... .......... .......... .......... .......... 5% 7.13M 19s
13650K .......... .......... .......... .......... .......... 5% 8.72M 19s
13700K .......... .......... .......... .......... .......... 5% 7.04M 19s
13750K .......... .......... .......... .......... .......... 5% 8.72M 19s
13800K .......... .......... .......... .......... .......... 5% 9.39M 19s
13850K .......... .......... .......... .......... .......... 5% 7.61M 20s
13900K .......... .......... .......... .......... .......... 5% 10.8M 20s
13950K .......... .......... .......... .......... .......... 5% 8.03M 20s
14000K .......... .......... .......... .......... .......... 5% 11.1M 20s
14050K .......... .......... .......... .......... .......... 5% 7.62M 20s
14100K .......... .......... .......... .......... .......... 5% 9.00M 20s
14150K .......... .......... .......... .......... .......... 5% 9.75M 20s
14200K .......... .......... .......... .......... .......... 5% 6.08M 20s
14250K .......... .......... .......... .......... .......... 5% 10.1M 20s
14300K .......... .......... .......... .......... .......... 5% 15.4M 20s
14350K .......... .......... .......... .......... .......... 5% 6.34M 20s
14400K .......... .......... .......... .......... .......... 5% 10.5M 20s
14450K .......... .......... .......... .......... .......... 5% 9.51M 20s
14500K .......... .......... .......... .......... .......... 5% 11.4M 20s
14550K .......... .......... .......... .......... .......... 5% 12.0M 20s
14600K .......... .......... .......... .......... .......... 5% 12.1M 20s
14650K .......... .......... .......... .......... .......... 5% 10.7M 20s
14700K .......... .......... .......... .......... .......... 5% 7.51M 20s
14750K .......... .......... .......... .......... .......... 5% 11.1M 20s
14800K .......... .......... .......... .......... .......... 5% 16.4M 20s
14850K .......... .......... .......... .......... .......... 5% 7.92M 20s
14900K .......... .......... .......... .......... .......... 5% 21.6M 20s
14950K .......... .......... .......... .......... .......... 5% 5.67M 20s
15000K .......... .......... .......... .......... .......... 5% 21.5M 20s
15050K .......... .......... .......... .......... .......... 5% 11.4M 20s
15100K .......... .......... .......... .......... .......... 5% 6.77M 20s
15150K .......... .......... .......... .......... .......... 5% 12.0M 20s
15200K .......... .......... .......... .......... .......... 5% 10.3M 20s
15250K .......... .......... .......... .......... .......... 5% 10.1M 20s
15300K .......... .......... .......... .......... .......... 5% 10.2M 20s
15350K .......... .......... .......... .......... .......... 5% 6.02M 20s
15400K .......... .......... .......... .......... .......... 5% 9.56M 20s
15450K .......... .......... .......... .......... .......... 5% 10.9M 20s
15500K .......... .......... .......... .......... .......... 5% 10.6M 20s
15550K .......... .......... .......... .......... .......... 5% 11.1M 20s
15600K .......... .......... .......... .......... .......... 5% 6.21M 20s
15650K .......... .......... .......... .......... .......... 5% 11.3M 20s
15700K .......... .......... .......... .......... .......... 5% 8.14M 20s
15750K .......... .......... .......... .......... .......... 5% 6.61M 20s
15800K .......... .......... .......... .......... .......... 5% 10.8M 20s
15850K .......... .......... .......... .......... .......... 5% 5.67M 20s
15900K .......... .......... .......... .......... .......... 6% 12.4M 20s
15950K .......... .......... .......... .......... .......... 6% 6.07M 20s
16000K .......... .......... .......... .......... .......... 6% 11.0M 20s
16050K .......... .......... .......... .......... .......... 6% 12.2M 20s
16100K .......... .......... .......... .......... .......... 6% 6.09M 20s
16150K .......... .......... .......... .......... .......... 6% 10.5M 20s
16200K .......... .......... .......... .......... .......... 6% 7.24M 20s
16250K .......... .......... .......... .......... .......... 6% 9.16M 20s
16300K .......... .......... .......... .......... .......... 6% 9.78M 20s
16350K .......... .......... .......... .......... .......... 6% 11.1M 20s
16400K .......... .......... .......... .......... .......... 6% 10.9M 20s
16450K .......... .......... .......... .......... .......... 6% 5.90M 20s
16500K .......... .......... .......... .......... .......... 6% 10.5M 20s
16550K .......... .......... .......... .......... .......... 6% 11.2M 20s
16600K .......... .......... .......... .......... .......... 6% 9.41M 20s
16650K .......... .......... .......... .......... .......... 6% 11.3M 20s
16700K .......... .......... .......... .......... .......... 6% 8.82M 20s
16750K .......... .......... .......... .......... .......... 6% 11.6M 20s
16800K .......... .......... .......... .......... .......... 6% 11.0M 20s
16850K .......... .......... .......... .......... .......... 6% 10.3M 20s
16900K .......... .......... .......... .......... .......... 6% 7.92M 21s
16950K .......... .......... .......... .......... .......... 6% 10.8M 21s
17000K .......... .......... .......... .......... .......... 6% 11.2M 21s
17050K .......... .......... .......... .......... .......... 6% 25.8M 20s
17100K .......... .......... .......... .......... .......... 6% 11.5M 20s
17150K .......... .......... .......... .......... .......... 6% 12.2M 20s
17200K .......... .......... .......... .......... .......... 6% 12.0M 20s
17250K .......... .......... .......... .......... .......... 6% 6.98M 21s
17300K .......... .......... .......... .......... .......... 6% 16.8M 20s
17350K .......... .......... .......... .......... .......... 6% 7.63M 21s
17400K .......... .......... .......... .......... .......... 6% 11.6M 21s
17450K .......... .......... .......... .......... .......... 6% 6.65M 21s
17500K .......... .......... .......... .......... .......... 6% 9.64M 21s
17550K .......... .......... .......... .......... .......... 6% 10.5M 21s
17600K .......... .......... .......... .......... .......... 6% 7.01M 21s
17650K .......... .......... .......... .......... .......... 6% 7.23M 21s
17700K .......... .......... .......... .......... .......... 6% 9.76M 21s
17750K .......... .......... .......... .......... .......... 6% 9.63M 21s
17800K .......... .......... .......... .......... .......... 6% 9.65M 21s
17850K .......... .......... .......... .......... .......... 6% 7.33M 21s
17900K .......... .......... .......... .......... .......... 6% 11.0M 21s
17950K .......... .......... .......... .......... .......... 6% 7.92M 21s
18000K .......... .......... .......... .......... .......... 6% 11.7M 21s
18050K .......... .......... .......... .......... .......... 6% 10.8M 21s
18100K .......... .......... .......... .......... .......... 6% 11.9M 21s
18150K .......... .......... .......... .......... .......... 6% 9.45M 21s
18200K .......... .......... .......... .......... .......... 6% 12.0M 21s
18250K .......... .......... .......... .......... .......... 6% 10.3M 21s
18300K .......... .......... .......... .......... .......... 6% 11.6M 21s
18350K .......... .......... .......... .......... .......... 6% 9.32M 21s
18400K .......... .......... .......... .......... .......... 6% 10.6M 21s
18450K .......... .......... .......... .......... .......... 6% 10.9M 21s
18500K .......... .......... .......... .......... .......... 6% 10.2M 21s
18550K .......... .......... .......... .......... .......... 6% 15.9M 21s
18600K .......... .......... .......... .......... .......... 7% 7.58M 21s
18650K .......... .......... .......... .......... .......... 7% 13.4M 21s
18700K .......... .......... .......... .......... .......... 7% 7.44M 21s
18750K .......... .......... .......... .......... .......... 7% 14.6M 21s
18800K .......... .......... .......... .......... .......... 7% 10.2M 21s
18850K .......... .......... .......... .......... .......... 7% 4.10M 21s
18900K .......... .......... .......... .......... .......... 7% 140M 21s
18950K .......... .......... .......... .......... .......... 7% 14.5M 21s
19000K .......... .......... .......... .......... .......... 7% 4.43M 21s
19050K .......... .......... .......... .......... .......... 7% 156M 21s
19100K .......... .......... .......... .......... .......... 7% 7.05M 21s
19150K .......... .......... .......... .......... .......... 7% 5.96M 21s
19200K .......... .......... .......... .......... .......... 7% 5.84M 21s
19250K .......... .......... .......... .......... .......... 7% 7.91M 21s
19300K .......... .......... .......... .......... .......... 7% 7.07M 21s
19350K .......... .......... .......... .......... .......... 7% 5.03M 21s
19400K .......... .......... .......... .......... .......... 7% 7.53M 21s
19450K .......... .......... .......... .......... .......... 7% 5.77M 21s
19500K .......... .......... .......... .......... .......... 7% 8.94M 21s
19550K .......... .......... .......... .......... .......... 7% 5.46M 21s
19600K .......... .......... .......... .......... .......... 7% 5.50M 21s
19650K .......... .......... .......... .......... .......... 7% 5.47M 21s
19700K .......... .......... .......... .......... .......... 7% 6.16M 21s
19750K .......... .......... .......... .......... .......... 7% 6.35M 21s
19800K .......... .......... .......... .......... .......... 7% 5.09M 21s
19850K .......... .......... .......... .......... .......... 7% 4.83M 21s
19900K .......... .......... .......... .......... .......... 7% 5.41M 22s
19950K .......... .......... .......... .......... .......... 7% 4.28M 22s
20000K .......... .......... .......... .......... .......... 7% 5.61M 22s
20050K .......... .......... .......... .......... .......... 7% 5.29M 22s
20100K .......... .......... .......... .......... .......... 7% 5.22M 22s
20150K .......... .......... .......... .......... .......... 7% 5.42M 22s
20200K .......... .......... .......... .......... .......... 7% 7.21M 22s
20250K .......... .......... .......... .......... .......... 7% 6.82M 22s
20300K .......... .......... .......... .......... .......... 7% 7.00M 22s
20350K .......... .......... .......... .......... .......... 7% 7.03M 22s
20400K .......... .......... .......... .......... .......... 7% 7.02M 22s
20450K .......... .......... .......... .......... .......... 7% 9.78M 22s
20500K .......... .......... .......... .......... .......... 7% 7.52M 22s
20550K .......... .......... .......... .......... .......... 7% 9.83M 22s
20600K .......... .......... .......... .......... .......... 7% 6.98M 22s
20650K .......... .......... .......... .......... .......... 7% 11.5M 22s
20700K .......... .......... .......... .......... .......... 7% 7.57M 22s
20750K .......... .......... .......... .......... .......... 7% 9.25M 22s
20800K .......... .......... .......... .......... .......... 7% 11.4M 22s
20850K .......... .......... .......... .......... .......... 7% 10.2M 22s
20900K .......... .......... .......... .......... .......... 7% 11.5M 22s
20950K .......... .......... .......... .......... .......... 7% 7.07M 22s
21000K .......... .......... .......... .......... .......... 7% 9.57M 22s
21050K .......... .......... .......... .......... .......... 7% 7.65M 22s
21100K .......... .......... .......... .......... .......... 7% 9.67M 22s
21150K .......... .......... .......... .......... .......... 7% 10.4M 22s
21200K .......... .......... .......... .......... .......... 7% 8.27M 22s
21250K .......... .......... .......... .......... .......... 8% 10.9M 22s
21300K .......... .......... .......... .......... .......... 8% 7.33M 22s
21350K .......... .......... .......... .......... .......... 8% 9.85M 22s
21400K .......... .......... .......... .......... .......... 8% 4.89M 22s
21450K .......... .......... .......... .......... .......... 8% 92.6M 22s
21500K .......... .......... .......... .......... .......... 8% 9.53M 22s
21550K .......... .......... .......... .......... .......... 8% 7.55M 22s
21600K .......... .......... .......... .......... .......... 8% 8.74M 22s
21650K .......... .......... .......... .......... .......... 8% 9.27M 22s
21700K .......... .......... .......... .......... .......... 8% 8.30M 22s
21750K .......... .......... .......... .......... .......... 8% 7.71M 22s
21800K .......... .......... .......... .......... .......... 8% 10.4M 22s
21850K .......... .......... .......... .......... .......... 8% 8.78M 22s
21900K .......... .......... .......... .......... .......... 8% 8.58M 22s
21950K .......... .......... .......... .......... .......... 8% 8.99M 22s
22000K .......... .......... .......... .......... .......... 8% 14.4M 22s
22050K .......... .......... .......... .......... .......... 8% 9.01M 22s
22100K .......... .......... .......... .......... .......... 8% 8.36M 22s
22150K .......... .......... .......... .......... .......... 8% 9.25M 22s
22200K .......... .......... .......... .......... .......... 8% 7.12M 22s
22250K .......... .......... .......... .......... .......... 8% 11.5M 22s
22300K .......... .......... .......... .......... .......... 8% 11.0M 22s
22350K .......... .......... .......... .......... .......... 8% 7.76M 22s
22400K .......... .......... .......... .......... .......... 8% 10.6M 22s
22450K .......... .......... .......... .......... .......... 8% 8.78M 22s
22500K .......... .......... .......... .......... .......... 8% 10.7M 22s
22550K .......... .......... .......... .......... .......... 8% 13.6M 22s
22600K .......... .......... .......... .......... .......... 8% 9.22M 22s
22650K .......... .......... .......... .......... .......... 8% 14.7M 22s
22700K .......... .......... .......... .......... .......... 8% 6.90M 22s
22750K .......... .......... .......... .......... .......... 8% 11.8M 22s
22800K .......... .......... .......... .......... .......... 8% 9.12M 22s
22850K .......... .......... .......... .......... .......... 8% 6.86M 22s
22900K .......... .......... .......... .......... .......... 8% 10.7M 22s
22950K .......... .......... .......... .......... .......... 8% 6.40M 22s
23000K .......... .......... .......... .......... .......... 8% 9.76M 22s
23050K .......... .......... .......... .......... .......... 8% 8.61M 22s
23100K .......... .......... .......... .......... .......... 8% 8.30M 22s
23150K .......... .......... .......... .......... .......... 8% 8.92M 22s
23200K .......... .......... .......... .......... .......... 8% 9.44M 22s
23250K .......... .......... .......... .......... .......... 8% 9.23M 22s
23300K .......... .......... .......... .......... .......... 8% 8.64M 22s
23350K .......... .......... .......... .......... .......... 8% 9.28M 22s
23400K .......... .......... .......... .......... .......... 8% 11.1M 22s
23450K .......... .......... .......... .......... .......... 8% 7.26M 22s
23500K .......... .......... .......... .......... .......... 8% 10.6M 22s
23550K .......... .......... .......... .......... .......... 8% 8.29M 22s
23600K .......... .......... .......... .......... .......... 8% 4.63M 22s
23650K .......... .......... .......... .......... .......... 8% 100M 22s
23700K .......... .......... .......... .......... .......... 8% 6.80M 22s
23750K .......... .......... .......... .......... .......... 8% 10.4M 22s
23800K .......... .......... .......... .......... .......... 8% 6.41M 22s
23850K .......... .......... .......... .......... .......... 8% 8.31M 22s
23900K .......... .......... .......... .......... .......... 9% 11.5M 22s
23950K .......... .......... .......... .......... .......... 9% 5.48M 22s
24000K .......... .......... .......... .......... .......... 9% 10.3M 22s
24050K .......... .......... .......... .......... .......... 9% 8.72M 22s
24100K .......... .......... .......... .......... .......... 9% 5.81M 22s
24150K .......... .......... .......... .......... .......... 9% 7.48M 22s
24200K .......... .......... .......... .......... .......... 9% 8.08M 22s
24250K .......... .......... .......... .......... .......... 9% 6.71M 22s
24300K .......... .......... .......... .......... .......... 9% 9.07M 22s
24350K .......... .......... .......... .......... .......... 9% 7.62M 22s
24400K .......... .......... .......... .......... .......... 9% 7.98M 22s
24450K .......... .......... .......... .......... .......... 9% 7.60M 22s
24500K .......... .......... .......... .......... .......... 9% 7.82M 22s
24550K .......... .......... .......... .......... .......... 9% 6.89M 22s
24600K .......... .......... .......... .......... .......... 9% 10.8M 22s
24650K .......... .......... .......... .......... .......... 9% 11.2M 22s
24700K .......... .......... .......... .......... .......... 9% 7.73M 22s
24750K .......... .......... .......... .......... .......... 9% 7.91M 23s
24800K .......... .......... .......... .......... .......... 9% 8.60M 23s
24850K .......... .......... .......... .......... .......... 9% 5.37M 23s
24900K .......... .......... .......... .......... .......... 9% 8.38M 23s
24950K .......... .......... .......... .......... .......... 9% 5.54M 23s
25000K .......... .......... .......... .......... .......... 9% 5.48M 23s
25050K .......... .......... .......... .......... .......... 9% 6.06M 23s
25100K .......... .......... .......... .......... .......... 9% 4.51M 23s
25150K .......... .......... .......... .......... .......... 9% 7.49M 23s
25200K .......... .......... .......... .......... .......... 9% 5.88M 23s
25250K .......... .......... .......... .......... .......... 9% 8.55M 23s
25300K .......... .......... .......... .......... .......... 9% 5.71M 23s
25350K .......... .......... .......... .......... .......... 9% 7.11M 23s
25400K .......... .......... .......... .......... .......... 9% 5.08M 23s
25450K .......... .......... .......... .......... .......... 9% 6.20M 23s
25500K .......... .......... .......... .......... .......... 9% 5.83M 23s
25550K .......... .......... .......... .......... .......... 9% 6.21M 23s
25600K .......... .......... .......... .......... .......... 9% 5.33M 23s
25650K .......... .......... .......... .......... .......... 9% 6.84M 23s
25700K .......... .......... .......... .......... .......... 9% 5.33M 23s
25750K .......... .......... .......... .......... .......... 9% 7.04M 23s
25800K .......... .......... .......... .......... .......... 9% 5.69M 23s
25850K .......... .......... .......... .......... .......... 9% 6.82M 23s
25900K .......... .......... .......... .......... .......... 9% 6.97M 23s
25950K .......... .......... .......... .......... .......... 9% 6.51M 23s
26000K .......... .......... .......... .......... .......... 9% 7.79M 23s
26050K .......... .......... .......... .......... .......... 9% 7.36M 23s
26100K .......... .......... .......... .......... .......... 9% 7.73M 23s
26150K .......... .......... .......... .......... .......... 9% 7.38M 23s
26200K .......... .......... .......... .......... .......... 9% 8.58M 23s
26250K .......... .......... .......... .......... .......... 9% 8.36M 23s
26300K .......... .......... .......... .......... .......... 9% 8.74M 23s
26350K .......... .......... .......... .......... .......... 9% 11.6M 23s
26400K .......... .......... .......... .......... .......... 9% 11.1M 23s
26450K .......... .......... .......... .......... .......... 9% 6.34M 23s
26500K .......... .......... .......... .......... .......... 9% 11.8M 23s
26550K .......... .......... .......... .......... .......... 10% 11.5M 23s
26600K .......... .......... .......... .......... .......... 10% 7.25M 23s
26650K .......... .......... .......... .......... .......... 10% 10.6M 23s
26700K .......... .......... .......... .......... .......... 10% 10.2M 23s
26750K .......... .......... .......... .......... .......... 10% 7.55M 23s
26800K .......... .......... .......... .......... .......... 10% 10.3M 23s
26850K .......... .......... .......... .......... .......... 10% 9.51M 23s
26900K .......... .......... .......... .......... .......... 10% 9.08M 23s
26950K .......... .......... .......... .......... .......... 10% 10.5M 23s
27000K .......... .......... .......... .......... .......... 10% 9.19M 23s
27050K .......... .......... .......... .......... .......... 10% 10.8M 23s
27100K .......... .......... .......... .......... .......... 10% 10.7M 23s
27150K .......... .......... .......... .......... .......... 10% 11.4M 23s
27200K .......... .......... .......... .......... .......... 10% 10.7M 23s
27250K .......... .......... .......... .......... .......... 10% 11.7M 23s
27300K .......... .......... .......... .......... .......... 10% 10.1M 23s
27350K .......... .......... .......... .......... .......... 10% 11.3M 23s
27400K .......... .......... .......... .......... .......... 10% 10.6M 23s
27450K .......... .......... .......... .......... .......... 10% 12.0M 23s
27500K .......... .......... .......... .......... .......... 10% 13.2M 23s
27550K .......... .......... .......... .......... .......... 10% 12.6M 23s
27600K .......... .......... .......... .......... .......... 10% 13.5M 23s
27650K .......... .......... .......... .......... .......... 10% 11.3M 23s
27700K .......... .......... .......... .......... .......... 10% 12.3M 23s
27750K .......... .......... .......... .......... .......... 10% 12.0M 23s
27800K .......... .......... .......... .......... .......... 10% 16.9M 23s
27850K .......... .......... .......... .......... .......... 10% 11.3M 23s
27900K .......... .......... .......... .......... .......... 10% 23.2M 23s
27950K .......... .......... .......... .......... .......... 10% 7.82M 23s
28000K .......... .......... .......... .......... .......... 10% 18.4M 23s
28050K .......... .......... .......... .......... .......... 10% 11.6M 23s
28100K .......... .......... .......... .......... .......... 10% 9.74M 23s
28150K .......... .......... .......... .......... .......... 10% 11.8M 23s
28200K .......... .......... .......... .......... .......... 10% 4.92M 23s
28250K .......... .......... .......... .......... .......... 10% 28.2M 23s
28300K .......... .......... .......... .......... .......... 10% 6.26M 23s
28350K .......... .......... .......... .......... .......... 10% 6.19M 23s
28400K .......... .......... .......... .......... .......... 10% 7.96M 23s
28450K .......... .......... .......... .......... .......... 10% 5.52M 23s
28500K .......... .......... .......... .......... .......... 10% 7.52M 23s
28550K .......... .......... .......... .......... .......... 10% 7.43M 23s
28600K .......... .......... .......... .......... .......... 10% 10.4M 23s
28650K .......... .......... .......... .......... .......... 10% 6.21M 23s
28700K .......... .......... .......... .......... .......... 10% 10.4M 23s
28750K .......... .......... .......... .......... .......... 10% 9.48M 23s
28800K .......... .......... .......... .......... .......... 10% 6.70M 23s
28850K .......... .......... .......... .......... .......... 10% 8.84M 23s
28900K .......... .......... .......... .......... .......... 10% 8.27M 23s
28950K .......... .......... .......... .......... .......... 10% 7.08M 23s
29000K .......... .......... .......... .......... .......... 10% 4.54M 23s
29050K .......... .......... .......... .......... .......... 10% 10.6M 23s
29100K .......... .......... .......... .......... .......... 10% 4.78M 23s
29150K .......... .......... .......... .......... .......... 10% 4.71M 23s
29200K .......... .......... .......... .......... .......... 11% 4.34M 23s
29250K .......... .......... .......... .......... .......... 11% 5.54M 23s
29300K .......... .......... .......... .......... .......... 11% 5.72M 23s
29350K .......... .......... .......... .......... .......... 11% 4.14M 23s
29400K .......... .......... .......... .......... .......... 11% 5.96M 23s
29450K .......... .......... .......... .......... .......... 11% 5.03M 23s
29500K .......... .......... .......... .......... .......... 11% 4.59M 23s
29550K .......... .......... .......... .......... .......... 11% 5.36M 23s
29600K .......... .......... .......... .......... .......... 11% 5.17M 23s
29650K .......... .......... .......... .......... .......... 11% 5.04M 23s
29700K .......... .......... .......... .......... .......... 11% 4.34M 24s
29750K .......... .......... .......... .......... .......... 11% 5.89M 24s
29800K .......... .......... .......... .......... .......... 11% 4.67M 24s
29850K .......... .......... .......... .......... .......... 11% 5.66M 24s
29900K .......... .......... .......... .......... .......... 11% 4.88M 24s
29950K .......... .......... .......... .......... .......... 11% 6.09M 24s
30000K .......... .......... .......... .......... .......... 11% 6.08M 24s
30050K .......... .......... .......... .......... .......... 11% 5.69M 24s
30100K .......... .......... .......... .......... .......... 11% 4.22M 24s
30150K .......... .......... .......... .......... .......... 11% 8.04M 24s
30200K .......... .......... .......... .......... .......... 11% 5.26M 24s
30250K .......... .......... .......... .......... .......... 11% 6.41M 24s
30300K .......... .......... .......... .......... .......... 11% 7.01M 24s
30350K .......... .......... .......... .......... .......... 11% 5.45M 24s
30400K .......... .......... .......... .......... .......... 11% 7.69M 24s
30450K .......... .......... .......... .......... .......... 11% 4.80M 24s
30500K .......... .......... .......... .......... .......... 11% 8.94M 24s
30550K .......... .......... .......... .......... .......... 11% 6.77M 24s
30600K .......... .......... .......... .......... .......... 11% 4.28M 24s
30650K .......... .......... .......... .......... .......... 11% 24.5M 24s
30700K .......... .......... .......... .......... .......... 11% 7.46M 24s
30750K .......... .......... .......... .......... .......... 11% 5.97M 24s
30800K .......... .......... .......... .......... .......... 11% 13.2M 24s
30850K .......... .......... .......... .......... .......... 11% 6.57M 24s
30900K .......... .......... .......... .......... .......... 11% 5.10M 24s
30950K .......... .......... .......... .......... .......... 11% 5.86M 24s
31000K .......... .......... .......... .......... .......... 11% 8.92M 24s
31050K .......... .......... .......... .......... .......... 11% 5.77M 24s
31100K .......... .......... .......... .......... .......... 11% 7.73M 24s
31150K .......... .......... .......... .......... .......... 11% 5.28M 24s
31200K .......... .......... .......... .......... .......... 11% 6.81M 24s
31250K .......... .......... .......... .......... .......... 11% 5.49M 24s
31300K .......... .......... .......... .......... .......... 11% 8.53M 24s
31350K .......... .......... .......... .......... .......... 11% 6.47M 24s
31400K .......... .......... .......... .......... .......... 11% 7.52M 24s
31450K .......... .......... .......... .......... .......... 11% 7.16M 24s
31500K .......... .......... .......... .......... .......... 11% 7.66M 24s
31550K .......... .......... .......... .......... .......... 11% 6.53M 24s
31600K .......... .......... .......... .......... .......... 11% 10.7M 24s
31650K .......... .......... .......... .......... .......... 11% 6.26M 24s
31700K .......... .......... .......... .......... .......... 11% 5.98M 24s
31750K .......... .......... .......... .......... .......... 11% 10.8M 24s
31800K .......... .......... .......... .......... .......... 11% 6.49M 24s
31850K .......... .......... .......... .......... .......... 12% 7.91M 24s
31900K .......... .......... .......... .......... .......... 12% 7.47M 24s
31950K .......... .......... .......... .......... .......... 12% 6.20M 24s
32000K .......... .......... .......... .......... .......... 12% 10.4M 24s
32050K .......... .......... .......... .......... .......... 12% 6.68M 24s
32100K .......... .......... .......... .......... .......... 12% 9.01M 24s
32150K .......... .......... .......... .......... .......... 12% 7.37M 24s
32200K .......... .......... .......... .......... .......... 12% 7.90M 24s
32250K .......... .......... .......... .......... .......... 12% 14.1M 24s
32300K .......... .......... .......... .......... .......... 12% 8.53M 24s
32350K .......... .......... .......... .......... .......... 12% 9.98M 24s
32400K .......... .......... .......... .......... .......... 12% 9.43M 24s
32450K .......... .......... .......... .......... .......... 12% 8.44M 24s
32500K .......... .......... .......... .......... .......... 12% 9.39M 24s
32550K .......... .......... .......... .......... .......... 12% 11.2M 24s
32600K .......... .......... .......... .......... .......... 12% 7.93M 24s
32650K .......... .......... .......... .......... .......... 12% 12.3M 24s
32700K .......... .......... .......... .......... .......... 12% 10.7M 24s
32750K .......... .......... .......... .......... .......... 12% 12.2M 24s
32800K .......... .......... .......... .......... .......... 12% 9.10M 24s
32850K .......... .......... .......... .......... .......... 12% 10.8M 24s
32900K .......... .......... .......... .......... .......... 12% 11.5M 24s
32950K .......... .......... .......... .......... .......... 12% 8.12M 24s
33000K .......... .......... .......... .......... .......... 12% 17.5M 24s
33050K .......... .......... .......... .......... .......... 12% 12.0M 24s
33100K .......... .......... .......... .......... .......... 12% 10.2M 24s
33150K .......... .......... .......... .......... .......... 12% 11.0M 24s
33200K .......... .......... .......... .......... .......... 12% 11.7M 24s
33250K .......... .......... .......... .......... .......... 12% 10.4M 24s
33300K .......... .......... .......... .......... .......... 12% 13.5M 24s
33350K .......... .......... .......... .......... .......... 12% 8.55M 24s
33400K .......... .......... .......... .......... .......... 12% 14.7M 24s
33450K .......... .......... .......... .......... .......... 12% 9.22M 24s
33500K .......... .......... .......... .......... .......... 12% 15.4M 24s
33550K .......... .......... .......... .......... .......... 12% 11.7M 24s
33600K .......... .......... .......... .......... .......... 12% 11.2M 24s
33650K .......... .......... .......... .......... .......... 12% 12.9M 24s
33700K .......... .......... .......... .......... .......... 12% 12.9M 24s
33750K .......... .......... .......... .......... .......... 12% 10.1M 24s
33800K .......... .......... .......... .......... .......... 12% 17.4M 24s
33850K .......... .......... .......... .......... .......... 12% 8.86M 24s
33900K .......... .......... .......... .......... .......... 12% 24.5M 24s
33950K .......... .......... .......... .......... .......... 12% 11.2M 24s
34000K .......... .......... .......... .......... .......... 12% 15.4M 24s
34050K .......... .......... .......... .......... .......... 12% 29.2M 24s
34100K .......... .......... .......... .......... .......... 12% 11.8M 24s
34150K .......... .......... .......... .......... .......... 12% 11.5M 24s
34200K .......... .......... .......... .......... .......... 12% 11.5M 24s
34250K .......... .......... .......... .......... .......... 12% 7.00M 24s
34300K .......... .......... .......... .......... .......... 12% 78.6M 24s
34350K .......... .......... .......... .......... .......... 12% 11.2M 24s
34400K .......... .......... .......... .......... .......... 12% 11.7M 24s
34450K .......... .......... .......... .......... .......... 12% 11.4M 24s
34500K .......... .......... .......... .......... .......... 12% 11.6M 24s
34550K .......... .......... .......... .......... .......... 13% 10.6M 24s
34600K .......... .......... .......... .......... .......... 13% 11.5M 24s
34650K .......... .......... .......... .......... .......... 13% 10.8M 24s
34700K .......... .......... .......... .......... .......... 13% 9.86M 24s
34750K .......... .......... .......... .......... .......... 13% 11.2M 24s
34800K .......... .......... .......... .......... .......... 13% 12.2M 24s
34850K .......... .......... .......... .......... .......... 13% 9.79M 24s
34900K .......... .......... .......... .......... .......... 13% 10.9M 24s
34950K .......... .......... .......... .......... .......... 13% 9.43M 24s
35000K .......... .......... .......... .......... .......... 13% 9.42M 24s
35050K .......... .......... .......... .......... .......... 13% 9.81M 24s
35100K .......... .......... .......... .......... .......... 13% 8.84M 24s
35150K .......... .......... .......... .......... .......... 13% 11.7M 24s
35200K .......... .......... .......... .......... .......... 13% 7.94M 24s
35250K .......... .......... .......... .......... .......... 13% 9.49M 24s
35300K .......... .......... .......... .......... .......... 13% 11.6M 24s
35350K .......... .......... .......... .......... .......... 13% 8.83M 24s
35400K .......... .......... .......... .......... .......... 13% 9.48M 23s
35450K .......... .......... .......... .......... .......... 13% 10.6M 23s
35500K .......... .......... .......... .......... .......... 13% 10.7M 23s
35550K .......... .......... .......... .......... .......... 13% 10.1M 23s
35600K .......... .......... .......... .......... .......... 13% 9.94M 23s
35650K .......... .......... .......... .......... .......... 13% 9.62M 23s
35700K .......... .......... .......... .......... .......... 13% 22.3M 23s
35750K .......... .......... .......... .......... .......... 13% 10.9M 23s
35800K .......... .......... .......... .......... .......... 13% 11.4M 23s
35850K .......... .......... .......... .......... .......... 13% 11.2M 23s
35900K .......... .......... .......... .......... .......... 13% 16.6M 23s
35950K .......... .......... .......... .......... .......... 13% 14.8M 23s
36000K .......... .......... .......... .......... .......... 13% 5.69M 23s
36050K .......... .......... .......... .......... .......... 13% 143M 23s
36100K .......... .......... .......... .......... .......... 13% 9.39M 23s
36150K .......... .......... .......... .......... .......... 13% 4.83M 23s
36200K .......... .......... .......... .......... .......... 13% 42.0M 23s
36250K .......... .......... .......... .......... .......... 13% 13.2M 23s
36300K .......... .......... .......... .......... .......... 13% 5.95M 23s
36350K .......... .......... .......... .......... .......... 13% 6.93M 23s
36400K .......... .......... .......... .......... .......... 13% 8.63M 23s
36450K .......... .......... .......... .......... .......... 13% 5.93M 23s
36500K .......... .......... .......... .......... .......... 13% 8.60M 23s
36550K .......... .......... .......... .......... .......... 13% 8.07M 23s
36600K .......... .......... .......... .......... .......... 13% 7.58M 23s
36650K .......... .......... .......... .......... .......... 13% 6.68M 23s
36700K .......... .......... .......... .......... .......... 13% 7.01M 23s
36750K .......... .......... .......... .......... .......... 13% 5.05M 23s
36800K .......... .......... .......... .......... .......... 13% 164M 23s
36850K .......... .......... .......... .......... .......... 13% 7.60M 23s
36900K .......... .......... .......... .......... .......... 13% 9.31M 23s
36950K .......... .......... .......... .......... .......... 13% 5.95M 23s
37000K .......... .......... .......... .......... .......... 13% 11.3M 23s
37050K .......... .......... .......... .......... .......... 13% 5.78M 23s
37100K .......... .......... .......... .......... .......... 13% 5.70M 23s
37150K .......... .......... .......... .......... .......... 13% 5.50M 23s
37200K .......... .......... .......... .......... .......... 14% 5.49M 23s
37250K .......... .......... .......... .......... .......... 14% 6.07M 23s
37300K .......... .......... .......... .......... .......... 14% 5.83M 23s
37350K .......... .......... .......... .......... .......... 14% 4.27M 24s
37400K .......... .......... .......... .......... .......... 14% 6.56M 24s
37450K .......... .......... .......... .......... .......... 14% 5.59M 24s
37500K .......... .......... .......... .......... .......... 14% 8.93M 24s
37550K .......... .......... .......... .......... .......... 14% 4.17M 24s
37600K .......... .......... .......... .......... .......... 14% 9.17M 24s
37650K .......... .......... .......... .......... .......... 14% 4.16M 24s
37700K .......... .......... .......... .......... .......... 14% 5.93M 24s
37750K .......... .......... .......... .......... .......... 14% 4.15M 24s
37800K .......... .......... .......... .......... .......... 14% 6.47M 24s
37850K .......... .......... .......... .......... .......... 14% 6.37M 24s
37900K .......... .......... .......... .......... .......... 14% 9.57M 24s
37950K .......... .......... .......... .......... .......... 14% 6.09M 24s
38000K .......... .......... .......... .......... .......... 14% 6.25M 24s
38050K .......... .......... .......... .......... .......... 14% 6.20M 24s
38100K .......... .......... .......... .......... .......... 14% 7.46M 24s
38150K .......... .......... .......... .......... .......... 14% 9.08M 24s
38200K .......... .......... .......... .......... .......... 14% 6.22M 24s
38250K .......... .......... .......... .......... .......... 14% 11.1M 24s
38300K .......... .......... .......... .......... .......... 14% 6.59M 24s
38350K .......... .......... .......... .......... .......... 14% 8.34M 24s
38400K .......... .......... .......... .......... .......... 14% 11.1M 24s
38450K .......... .......... .......... .......... .......... 14% 7.41M 24s
38500K .......... .......... .......... .......... .......... 14% 7.30M 24s
38550K .......... .......... .......... .......... .......... 14% 6.86M 24s
38600K .......... .......... .......... .......... .......... 14% 6.21M 24s
38650K .......... .......... .......... .......... .......... 14% 8.87M 24s
38700K .......... .......... .......... .......... .......... 14% 6.29M 24s
38750K .......... .......... .......... .......... .......... 14% 6.89M 24s
38800K .......... .......... .......... .......... .......... 14% 5.73M 24s
38850K .......... .......... .......... .......... .......... 14% 5.37M 24s
38900K .......... .......... .......... .......... .......... 14% 8.12M 24s
38950K .......... .......... .......... .......... .......... 14% 6.90M 24s
39000K .......... .......... .......... .......... .......... 14% 9.32M 24s
39050K .......... .......... .......... .......... .......... 14% 11.1M 24s
39100K .......... .......... .......... .......... .......... 14% 5.67M 24s
39150K .......... .......... .......... .......... .......... 14% 10.7M 24s
39200K .......... .......... .......... .......... .......... 14% 5.96M 24s
39250K .......... .......... .......... .......... .......... 14% 10.7M 24s
39300K .......... .......... .......... .......... .......... 14% 8.07M 24s
39350K .......... .......... .......... .......... .......... 14% 7.22M 24s
39400K .......... .......... .......... .......... .......... 14% 10.9M 24s
39450K .......... .......... .......... .......... .......... 14% 6.05M 24s
39500K .......... .......... .......... .......... .......... 14% 25.1M 24s
39550K .......... .......... .......... .......... .......... 14% 6.86M 24s
39600K .......... .......... .......... .......... .......... 14% 6.07M 24s
39650K .......... .......... .......... .......... .......... 14% 7.00M 24s
39700K .......... .......... .......... .......... .......... 14% 5.63M 24s
39750K .......... .......... .......... .......... .......... 14% 8.59M 24s
39800K .......... .......... .......... .......... .......... 14% 6.38M 24s
39850K .......... .......... .......... .......... .......... 15% 6.67M 24s
39900K .......... .......... .......... .......... .......... 15% 9.81M 24s
39950K .......... .......... .......... .......... .......... 15% 5.61M 24s
40000K .......... .......... .......... .......... .......... 15% 6.59M 24s
40050K .......... .......... .......... .......... .......... 15% 8.66M 24s
40100K .......... .......... .......... .......... .......... 15% 9.54M 24s
40150K .......... .......... .......... .......... .......... 15% 9.39M 24s
40200K .......... .......... .......... .......... .......... 15% 9.13M 24s
40250K .......... .......... .......... .......... .......... 15% 8.22M 24s
40300K .......... .......... .......... .......... .......... 15% 9.61M 24s
40350K .......... .......... .......... .......... .......... 15% 7.73M 24s
40400K .......... .......... .......... .......... .......... 15% 10.4M 24s
40450K .......... .......... .......... .......... .......... 15% 8.21M 24s
40500K .......... .......... .......... .......... .......... 15% 9.62M 24s
40550K .......... .......... .......... .......... .......... 15% 10.8M 24s
40600K .......... .......... .......... .......... .......... 15% 6.78M 24s
40650K .......... .......... .......... .......... .......... 15% 10.8M 24s
40700K .......... .......... .......... .......... .......... 15% 10.7M 24s
40750K .......... .......... .......... .......... .......... 15% 11.1M 24s
40800K .......... .......... .......... .......... .......... 15% 10.9M 24s
40850K .......... .......... .......... .......... .......... 15% 12.3M 24s
40900K .......... .......... .......... .......... .......... 15% 13.3M 24s
40950K .......... .......... .......... .......... .......... 15% 12.8M 24s
41000K .......... .......... .......... .......... .......... 15% 12.6M 24s
41050K .......... .......... .......... .......... .......... 15% 19.7M 24s
41100K .......... .......... .......... .......... .......... 15% 8.53M 24s
41150K .......... .......... .......... .......... .......... 15% 13.4M 24s
41200K .......... .......... .......... .......... .......... 15% 12.4M 24s
41250K .......... .......... .......... .......... .......... 15% 12.1M 24s
41300K .......... .......... .......... .......... .......... 15% 14.3M 24s
41350K .......... .......... .......... .......... .......... 15% 9.13M 24s
41400K .......... .......... .......... .......... .......... 15% 14.1M 24s
41450K .......... .......... .......... .......... .......... 15% 11.7M 24s
41500K .......... .......... .......... .......... .......... 15% 11.1M 24s
41550K .......... .......... .......... .......... .......... 15% 12.6M 24s
41600K .......... .......... .......... .......... .......... 15% 13.0M 24s
41650K .......... .......... .......... .......... .......... 15% 12.9M 23s
41700K .......... .......... .......... .......... .......... 15% 12.0M 23s
41750K .......... .......... .......... .......... .......... 15% 15.4M 23s
41800K .......... .......... .......... .......... .......... 15% 15.7M 23s
41850K .......... .......... .......... .......... .......... 15% 13.9M 23s
41900K .......... .......... .......... .......... .......... 15% 11.1M 23s
41950K .......... .......... .......... .......... .......... 15% 9.71M 23s
42000K .......... .......... .......... .......... .......... 15% 13.7M 23s
42050K .......... .......... .......... .......... .......... 15% 36.0M 23s
42100K .......... .......... .......... .......... .......... 15% 12.7M 23s
42150K .......... .......... .......... .......... .......... 15% 11.9M 23s
42200K .......... .......... .......... .......... .......... 15% 12.9M 23s
42250K .......... .......... .......... .......... .......... 15% 14.9M 23s
42300K .......... .......... .......... .......... .......... 15% 32.5M 23s
42350K .......... .......... .......... .......... .......... 15% 12.3M 23s
42400K .......... .......... .......... .......... .......... 15% 14.2M 23s
42450K .......... .......... .......... .......... .......... 15% 6.73M 23s
42500K .......... .......... .......... .......... .......... 16% 28.2M 23s
42550K .......... .......... .......... .......... .......... 16% 42.0M 23s
42600K .......... .......... .......... .......... .......... 16% 14.2M 23s
42650K .......... .......... .......... .......... .......... 16% 11.5M 23s
42700K .......... .......... .......... .......... .......... 16% 13.5M 23s
42750K .......... .......... .......... .......... .......... 16% 11.2M 23s
42800K .......... .......... .......... .......... .......... 16% 13.3M 23s
42850K .......... .......... .......... .......... .......... 16% 11.0M 23s
42900K .......... .......... .......... .......... .......... 16% 12.1M 23s
42950K .......... .......... .......... .......... .......... 16% 11.5M 23s
43000K .......... .......... .......... .......... .......... 16% 12.0M 23s
43050K .......... .......... .......... .......... .......... 16% 10.9M 23s
43100K .......... .......... .......... .......... .......... 16% 10.7M 23s
43150K .......... .......... .......... .......... .......... 16% 11.5M 23s
43200K .......... .......... .......... .......... .......... 16% 9.98M 23s
43250K .......... .......... .......... .......... .......... 16% 16.8M 23s
43300K .......... .......... .......... .......... .......... 16% 10.7M 23s
43350K .......... .......... .......... .......... .......... 16% 12.7M 23s
43400K .......... .......... .......... .......... .......... 16% 12.0M 23s
43450K .......... .......... .......... .......... .......... 16% 11.9M 23s
43500K .......... .......... .......... .......... .......... 16% 14.7M 23s
43550K .......... .......... .......... .......... .......... 16% 12.7M 23s
43600K .......... .......... .......... .......... .......... 16% 11.2M 23s
43650K .......... .......... .......... .......... .......... 16% 11.5M 23s
43700K .......... .......... .......... .......... .......... 16% 10.3M 23s
43750K .......... .......... .......... .......... .......... 16% 13.8M 23s
43800K .......... .......... .......... .......... .......... 16% 12.1M 23s
43850K .......... .......... .......... .......... .......... 16% 7.14M 23s
43900K .......... .......... .......... .......... .......... 16% 25.3M 23s
43950K .......... .......... .......... .......... .......... 16% 6.77M 23s
44000K .......... .......... .......... .......... .......... 16% 12.9M 23s
44050K .......... .......... .......... .......... .......... 16% 10.8M 23s
44100K .......... .......... .......... .......... .......... 16% 9.03M 23s
44150K .......... .......... .......... .......... .......... 16% 11.8M 23s
44200K .......... .......... .......... .......... .......... 16% 9.94M 23s
44250K .......... .......... .......... .......... .......... 16% 7.92M 23s
44300K .......... .......... .......... .......... .......... 16% 12.4M 23s
44350K .......... .......... .......... .......... .......... 16% 9.70M 23s
44400K .......... .......... .......... .......... .......... 16% 13.1M 23s
44450K .......... .......... .......... .......... .......... 16% 10.5M 23s
44500K .......... .......... .......... .......... .......... 16% 11.6M 23s
44550K .......... .......... .......... .......... .......... 16% 12.0M 23s
44600K .......... .......... .......... .......... .......... 16% 12.6M 23s
44650K .......... .......... .......... .......... .......... 16% 7.55M 23s
44700K .......... .......... .......... .......... .......... 16% 9.96M 23s
44750K .......... .......... .......... .......... .......... 16% 7.91M 23s
44800K .......... .......... .......... .......... .......... 16% 14.3M 23s
44850K .......... .......... .......... .......... .......... 16% 7.29M 23s
44900K .......... .......... .......... .......... .......... 16% 8.46M 23s
44950K .......... .......... .......... .......... .......... 16% 10.9M 23s
45000K .......... .......... .......... .......... .......... 16% 6.82M 23s
45050K .......... .......... .......... .......... .......... 16% 10.0M 23s
45100K .......... .......... .......... .......... .......... 16% 8.79M 23s
45150K .......... .......... .......... .......... .......... 17% 7.96M 23s
45200K .......... .......... .......... .......... .......... 17% 7.62M 23s
45250K .......... .......... .......... .......... .......... 17% 10.3M 23s
45300K .......... .......... .......... .......... .......... 17% 4.99M 23s
45350K .......... .......... .......... .......... .......... 17% 19.4M 23s
45400K .......... .......... .......... .......... .......... 17% 7.16M 23s
45450K .......... .......... .......... .......... .......... 17% 6.22M 23s
45500K .......... .......... .......... .......... .......... 17% 9.41M 23s
45550K .......... .......... .......... .......... .......... 17% 6.16M 23s
45600K .......... .......... .......... .......... .......... 17% 5.60M 23s
45650K .......... .......... .......... .......... .......... 17% 7.37M 23s
45700K .......... .......... .......... .......... .......... 17% 7.73M 23s
45750K .......... .......... .......... .......... .......... 17% 7.16M 23s
45800K .......... .......... .......... .......... .......... 17% 8.74M 23s
45850K .......... .......... .......... .......... .......... 17% 6.41M 23s
45900K .......... .......... .......... .......... .......... 17% 9.60M 23s
45950K .......... .......... .......... .......... .......... 17% 7.54M 23s
46000K .......... .......... .......... .......... .......... 17% 7.19M 23s
46050K .......... .......... .......... .......... .......... 17% 10.5M 23s
46100K .......... .......... .......... .......... .......... 17% 6.44M 23s
46150K .......... .......... .......... .......... .......... 17% 8.63M 23s
46200K .......... .......... .......... .......... .......... 17% 10.6M 23s
46250K .......... .......... .......... .......... .......... 17% 11.3M 23s
46300K .......... .......... .......... .......... .......... 17% 11.4M 23s
46350K .......... .......... .......... .......... .......... 17% 8.10M 23s
46400K .......... .......... .......... .......... .......... 17% 8.53M 23s
46450K .......... .......... .......... .......... .......... 17% 9.33M 23s
46500K .......... .......... .......... .......... .......... 17% 12.4M 23s
46550K .......... .......... .......... .......... .......... 17% 11.2M 23s
46600K .......... .......... .......... .......... .......... 17% 6.06M 23s
46650K .......... .......... .......... .......... .......... 17% 15.1M 23s
46700K .......... .......... .......... .......... .......... 17% 10.9M 23s
46750K .......... .......... .......... .......... .......... 17% 9.06M 23s
46800K .......... .......... .......... .......... .......... 17% 7.93M 23s
46850K .......... .......... .......... .......... .......... 17% 6.12M 23s
46900K .......... .......... .......... .......... .......... 17% 12.1M 23s
46950K .......... .......... .......... .......... .......... 17% 7.22M 23s
47000K .......... .......... .......... .......... .......... 17% 7.80M 23s
47050K .......... .......... .......... .......... .......... 17% 10.9M 23s
47100K .......... .......... .......... .......... .......... 17% 7.46M 23s
47150K .......... .......... .......... .......... .......... 17% 7.39M 23s
47200K .......... .......... .......... .......... .......... 17% 9.74M 23s
47250K .......... .......... .......... .......... .......... 17% 10.7M 23s
47300K .......... .......... .......... .......... .......... 17% 9.37M 23s
47350K .......... .......... .......... .......... .......... 17% 8.64M 23s
47400K .......... .......... .......... .......... .......... 17% 10.0M 23s
47450K .......... .......... .......... .......... .......... 17% 4.77M 23s
47500K .......... .......... .......... .......... .......... 17% 18.0M 23s
47550K .......... .......... .......... .......... .......... 17% 7.96M 23s
47600K .......... .......... .......... .......... .......... 17% 5.71M 23s
47650K .......... .......... .......... .......... .......... 17% 11.8M 23s
47700K .......... .......... .......... .......... .......... 17% 5.97M 23s
47750K .......... .......... .......... .......... .......... 17% 7.86M 23s
47800K .......... .......... .......... .......... .......... 18% 8.28M 23s
47850K .......... .......... .......... .......... .......... 18% 7.51M 23s
47900K .......... .......... .......... .......... .......... 18% 8.33M 23s
47950K .......... .......... .......... .......... .......... 18% 10.1M 23s
48000K .......... .......... .......... .......... .......... 18% 5.25M 23s
48050K .......... .......... .......... .......... .......... 18% 8.57M 23s
48100K .......... .......... .......... .......... .......... 18% 6.70M 23s
48150K .......... .......... .......... .......... .......... 18% 3.65M 23s
48200K .......... .......... .......... .......... .......... 18% 12.1M 23s
48250K .......... .......... .......... .......... .......... 18% 5.89M 23s
48300K .......... .......... .......... .......... .......... 18% 5.98M 23s
48350K .......... .......... .......... .......... .......... 18% 6.77M 23s
48400K .......... .......... .......... .......... .......... 18% 4.87M 23s
48450K .......... .......... .......... .......... .......... 18% 5.73M 23s
48500K .......... .......... .......... .......... .......... 18% 4.66M 23s
48550K .......... .......... .......... .......... .......... 18% 6.97M 23s
48600K .......... .......... .......... .......... .......... 18% 3.07M 23s
48650K .......... .......... .......... .......... .......... 18% 2.93M 23s
48700K .......... .......... .......... .......... .......... 18% 2.23M 23s
48750K .......... .......... .......... .......... .......... 18% 6.47M 23s
48800K .......... .......... .......... .......... .......... 18% 11.2M 23s
48850K .......... .......... .......... .......... .......... 18% 6.46M 23s
48900K .......... .......... .......... .......... .......... 18% 9.81M 23s
48950K .......... .......... .......... .......... .......... 18% 5.32M 23s
49000K .......... .......... .......... .......... .......... 18% 8.45M 23s
49050K .......... .......... .......... .......... .......... 18% 5.45M 23s
49100K .......... .......... .......... .......... .......... 18% 4.61M 23s
49150K .......... .......... .......... .......... .......... 18% 6.15M 23s
49200K .......... .......... .......... .......... .......... 18% 2.72M 23s
49250K .......... .......... .......... .......... .......... 18% 1.92M 23s
49300K .......... .......... .......... .......... .......... 18% 1.45M 23s
49350K .......... .......... .......... .......... .......... 18% 1.36M 23s
49400K .......... .......... .......... .......... .......... 18% 2.39M 23s
49450K .......... .......... .......... .......... .......... 18% 2.49M 24s
49500K .......... .......... .......... .......... .......... 18% 6.92M 24s
49550K .......... .......... .......... .......... .......... 18% 6.67M 24s
49600K .......... .......... .......... .......... .......... 18% 3.42M 24s
49650K .......... .......... .......... .......... .......... 18% 4.62M 24s
49700K .......... .......... .......... .......... .......... 18% 4.39M 24s
49750K .......... .......... .......... .......... .......... 18% 4.53M 24s
49800K .......... .......... .......... .......... .......... 18% 7.89M 24s
49850K .......... .......... .......... .......... .......... 18% 5.32M 24s
49900K .......... .......... .......... .......... .......... 18% 5.70M 24s
49950K .......... .......... .......... .......... .......... 18% 5.97M 24s
50000K .......... .......... .......... .......... .......... 18% 6.29M 24s
50050K .......... .......... .......... .......... .......... 18% 72.7M 24s
50100K .......... .......... .......... .......... .......... 18% 9.54M 24s
50150K .......... .......... .......... .......... .......... 18% 12.5M 24s
50200K .......... .......... .......... .......... .......... 18% 8.33M 24s
50250K .......... .......... .......... .......... .......... 18% 4.74M 24s
50300K .......... .......... .......... .......... .......... 18% 6.11M 24s
50350K .......... .......... .......... .......... .......... 18% 3.49M 24s
50400K .......... .......... .......... .......... .......... 18% 3.39M 24s
50450K .......... .......... .......... .......... .......... 19% 1.96M 24s
50500K .......... .......... .......... .......... .......... 19% 2.04M 24s
50550K .......... .......... .......... .......... .......... 19% 2.03M 24s
50600K .......... .......... .......... .......... .......... 19% 5.20M 24s
50650K .......... .......... .......... .......... .......... 19% 90.9M 24s
50700K .......... .......... .......... .......... .......... 19% 13.6M 24s
50750K .......... .......... .......... .......... .......... 19% 10.1M 24s
50800K .......... .......... .......... .......... .......... 19% 9.28M 24s
50850K .......... .......... .......... .......... .......... 19% 8.39M 24s
50900K .......... .......... .......... .......... .......... 19% 9.19M 24s
50950K .......... .......... .......... .......... .......... 19% 8.07M 24s
51000K .......... .......... .......... .......... .......... 19% 9.54M 24s
51050K .......... .......... .......... .......... .......... 19% 10.1M 24s
51100K .......... .......... .......... .......... .......... 19% 6.40M 24s
51150K .......... .......... .......... .......... .......... 19% 84.6M 24s
51200K .......... .......... .......... .......... .......... 19% 12.0M 24s
51250K .......... .......... .......... .......... .......... 19% 17.7M 24s
51300K .......... .......... .......... .......... .......... 19% 12.1M 24s
51350K .......... .......... .......... .......... .......... 19% 16.7M 24s
51400K .......... .......... .......... .......... .......... 19% 13.0M 24s
51450K .......... .......... .......... .......... .......... 19% 17.2M 24s
51500K .......... .......... .......... .......... .......... 19% 12.7M 24s
51550K .......... .......... .......... .......... .......... 19% 9.89M 24s
51600K .......... .......... .......... .......... .......... 19% 8.57M 24s
51650K .......... .......... .......... .......... .......... 19% 18.6M 24s
51700K .......... .......... .......... .......... .......... 19% 7.33M 24s
51750K .......... .......... .......... .......... .......... 19% 12.1M 24s
51800K .......... .......... .......... .......... .......... 19% 7.92M 24s
51850K .......... .......... .......... .......... .......... 19% 8.46M 24s
51900K .......... .......... .......... .......... .......... 19% 8.14M 24s
51950K .......... .......... .......... .......... .......... 19% 7.14M 24s
52000K .......... .......... .......... .......... .......... 19% 10.7M 24s
52050K .......... .......... .......... .......... .......... 19% 11.4M 24s
52100K .......... .......... .......... .......... .......... 19% 16.5M 24s
52150K .......... .......... .......... .......... .......... 19% 25.0M 24s
52200K .......... .......... .......... .......... .......... 19% 20.5M 24s
52250K .......... .......... .......... .......... .......... 19% 23.8M 24s
52300K .......... .......... .......... .......... .......... 19% 9.39M 24s
52350K .......... .......... .......... .......... .......... 19% 120M 23s
52400K .......... .......... .......... .......... .......... 19% 13.6M 23s
52450K .......... .......... .......... .......... .......... 19% 33.1M 23s
52500K .......... .......... .......... .......... .......... 19% 14.0M 23s
52550K .......... .......... .......... .......... .......... 19% 8.66M 23s
52600K .......... .......... .......... .......... .......... 19% 20.2M 23s
52650K .......... .......... .......... .......... .......... 19% 7.11M 23s
52700K .......... .......... .......... .......... .......... 19% 16.3M 23s
52750K .......... .......... .......... .......... .......... 19% 9.91M 23s
52800K .......... .......... .......... .......... .......... 19% 10.4M 23s
52850K .......... .......... .......... .......... .......... 19% 8.85M 23s
52900K .......... .......... .......... .......... .......... 19% 11.5M 23s
52950K .......... .......... .......... .......... .......... 19% 7.61M 23s
53000K .......... .......... .......... .......... .......... 19% 12.5M 23s
53050K .......... .......... .......... .......... .......... 19% 8.31M 23s
53100K .......... .......... .......... .......... .......... 19% 10.4M 23s
53150K .......... .......... .......... .......... .......... 20% 11.0M 23s
53200K .......... .......... .......... .......... .......... 20% 11.8M 23s
53250K .......... .......... .......... .......... .......... 20% 10.4M 23s
53300K .......... .......... .......... .......... .......... 20% 7.64M 23s
53350K .......... .......... .......... .......... .......... 20% 5.91M 23s
53400K .......... .......... .......... .......... .......... 20% 7.87M 23s
53450K .......... .......... .......... .......... .......... 20% 8.58M 23s
53500K .......... .......... .......... .......... .......... 20% 13.2M 23s
53550K .......... .......... .......... .......... .......... 20% 7.08M 23s
53600K .......... .......... .......... .......... .......... 20% 8.58M 23s
53650K .......... .......... .......... .......... .......... 20% 11.7M 23s
53700K .......... .......... .......... .......... .......... 20% 5.15M 23s
53750K .......... .......... .......... .......... .......... 20% 9.75M 23s
53800K .......... .......... .......... .......... .......... 20% 7.21M 23s
53850K .......... .......... .......... .......... .......... 20% 7.26M 23s
53900K .......... .......... .......... .......... .......... 20% 7.67M 23s
53950K .......... .......... .......... .......... .......... 20% 5.59M 23s
54000K .......... .......... .......... .......... .......... 20% 4.94M 23s
54050K .......... .......... .......... .......... .......... 20% 6.02M 23s
54100K .......... .......... .......... .......... .......... 20% 4.20M 23s
54150K .......... .......... .......... .......... .......... 20% 6.02M 23s
54200K .......... .......... .......... .......... .......... 20% 3.79M 23s
54250K .......... .......... .......... .......... .......... 20% 5.72M 23s
54300K .......... .......... .......... .......... .......... 20% 7.20M 23s
54350K .......... .......... .......... .......... .......... 20% 8.79M 23s
54400K .......... .......... .......... .......... .......... 20% 9.17M 23s
54450K .......... .......... .......... .......... .......... 20% 9.32M 23s
54500K .......... .......... .......... .......... .......... 20% 5.35M 23s
54550K .......... .......... .......... .......... .......... 20% 11.3M 23s
54600K .......... .......... .......... .......... .......... 20% 5.38M 23s
54650K .......... .......... .......... .......... .......... 20% 6.10M 23s
54700K .......... .......... .......... .......... .......... 20% 4.97M 23s
54750K .......... .......... .......... .......... .......... 20% 6.10M 23s
54800K .......... .......... .......... .......... .......... 20% 4.51M 23s
54850K .......... .......... .......... .......... .......... 20% 5.70M 23s
54900K .......... .......... .......... .......... .......... 20% 3.94M 23s
54950K .......... .......... .......... .......... .......... 20% 5.06M 23s
55000K .......... .......... .......... .......... .......... 20% 7.69M 23s
55050K .......... .......... .......... .......... .......... 20% 4.68M 23s
55100K .......... .......... .......... .......... .......... 20% 3.77M 23s
55150K .......... .......... .......... .......... .......... 20% 4.79M 23s
55200K .......... .......... .......... .......... .......... 20% 4.84M 23s
55250K .......... .......... .......... .......... .......... 20% 10.7M 23s
55300K .......... .......... .......... .......... .......... 20% 23.5M 23s
55350K .......... .......... .......... .......... .......... 20% 6.92M 23s
55400K .......... .......... .......... .......... .......... 20% 16.3M 23s
55450K .......... .......... .......... .......... .......... 20% 8.80M 23s
55500K .......... .......... .......... .......... .......... 20% 12.9M 23s
55550K .......... .......... .......... .......... .......... 20% 9.60M 23s
55600K .......... .......... .......... .......... .......... 20% 9.44M 23s
55650K .......... .......... .......... .......... .......... 20% 10.5M 23s
55700K .......... .......... .......... .......... .......... 20% 9.53M 23s
55750K .......... .......... .......... .......... .......... 20% 14.6M 23s
55800K .......... .......... .......... .......... .......... 21% 19.7M 23s
55850K .......... .......... .......... .......... .......... 21% 10.9M 23s
55900K .......... .......... .......... .......... .......... 21% 35.1M 23s
55950K .......... .......... .......... .......... .......... 21% 29.7M 23s
56000K .......... .......... .......... .......... .......... 21% 25.8M 23s
56050K .......... .......... .......... .......... .......... 21% 17.3M 23s
56100K .......... .......... .......... .......... .......... 21% 9.09M 23s
56150K .......... .......... .......... .......... .......... 21% 30.6M 23s
56200K .......... .......... .......... .......... .......... 21% 15.7M 23s
56250K .......... .......... .......... .......... .......... 21% 12.4M 23s
56300K .......... .......... .......... .......... .......... 21% 17.5M 23s
56350K .......... .......... .......... .......... .......... 21% 7.01M 23s
56400K .......... .......... .......... .......... .......... 21% 4.01M 23s
56450K .......... .......... .......... .......... .......... 21% 2.62M 23s
56500K .......... .......... .......... .......... .......... 21% 4.05M 23s
56550K .......... .......... .......... .......... .......... 21% 4.00M 23s
56600K .......... .......... .......... .......... .......... 21% 9.90M 23s
56650K .......... .......... .......... .......... .......... 21% 15.8M 23s
56700K .......... .......... .......... .......... .......... 21% 15.4M 23s
56750K .......... .......... .......... .......... .......... 21% 16.7M 23s
56800K .......... .......... .......... .......... .......... 21% 17.1M 23s
56850K .......... .......... .......... .......... .......... 21% 11.7M 23s
56900K .......... .......... .......... .......... .......... 21% 14.4M 23s
56950K .......... .......... .......... .......... .......... 21% 7.11M 23s
57000K .......... .......... .......... .......... .......... 21% 6.45M 23s
57050K .......... .......... .......... .......... .......... 21% 5.34M 23s
57100K .......... .......... .......... .......... .......... 21% 5.04M 23s
57150K .......... .......... .......... .......... .......... 21% 6.52M 23s
57200K .......... .......... .......... .......... .......... 21% 5.82M 23s
57250K .......... .......... .......... .......... .......... 21% 7.15M 23s
57300K .......... .......... .......... .......... .......... 21% 5.97M 23s
57350K .......... .......... .......... .......... .......... 21% 6.79M 23s
57400K .......... .......... .......... .......... .......... 21% 6.20M 23s
57450K .......... .......... .......... .......... .......... 21% 5.36M 23s
57500K .......... .......... .......... .......... .......... 21% 6.61M 23s
57550K .......... .......... .......... .......... .......... 21% 4.96M 23s
57600K .......... .......... .......... .......... .......... 21% 10.6M 23s
57650K .......... .......... .......... .......... .......... 21% 9.78M 23s
57700K .......... .......... .......... .......... .......... 21% 7.71M 23s
57750K .......... .......... .......... .......... .......... 21% 12.1M 23s
57800K .......... .......... .......... .......... .......... 21% 7.14M 23s
57850K .......... .......... .......... .......... .......... 21% 10.9M 23s
57900K .......... .......... .......... .......... .......... 21% 10.1M 23s
57950K .......... .......... .......... .......... .......... 21% 13.1M 23s
58000K .......... .......... .......... .......... .......... 21% 10.5M 23s
58050K .......... .......... .......... .......... .......... 21% 34.0M 23s
58100K .......... .......... .......... .......... .......... 21% 15.4M 23s
58150K .......... .......... .......... .......... .......... 21% 13.3M 23s
58200K .......... .......... .......... .......... .......... 21% 11.7M 23s
58250K .......... .......... .......... .......... .......... 21% 7.47M 23s
58300K .......... .......... .......... .......... .......... 21% 5.60M 23s
58350K .......... .......... .......... .......... .......... 21% 884K 23s
58400K .......... .......... .......... .......... .......... 21% 15.6M 23s
58450K .......... .......... .......... .......... .......... 22% 15.8M 23s
58500K .......... .......... .......... .......... .......... 22% 15.5M 23s
58550K .......... .......... .......... .......... .......... 22% 12.4M 23s
58600K .......... .......... .......... .......... .......... 22% 8.59M 23s
58650K .......... .......... .......... .......... .......... 22% 11.8M 23s
58700K .......... .......... .......... .......... .......... 22% 7.96M 23s
58750K .......... .......... .......... .......... .......... 22% 15.0M 23s
58800K .......... .......... .......... .......... .......... 22% 16.3M 23s
58850K .......... .......... .......... .......... .......... 22% 13.3M 23s
58900K .......... .......... .......... .......... .......... 22% 10.1M 23s
58950K .......... .......... .......... .......... .......... 22% 13.0M 23s
59000K .......... .......... .......... .......... .......... 22% 18.1M 23s
59050K .......... .......... .......... .......... .......... 22% 11.6M 23s
59100K .......... .......... .......... .......... .......... 22% 7.18M 23s
59150K .......... .......... .......... .......... .......... 22% 8.13M 23s
59200K .......... .......... .......... .......... .......... 22% 6.75M 23s
59250K .......... .......... .......... .......... .......... 22% 6.96M 23s
59300K .......... .......... .......... .......... .......... 22% 7.01M 23s
59350K .......... .......... .......... .......... .......... 22% 5.41M 23s
59400K .......... .......... .......... .......... .......... 22% 13.2M 23s
59450K .......... .......... .......... .......... .......... 22% 19.4M 23s
59500K .......... .......... .......... .......... .......... 22% 27.0M 23s
59550K .......... .......... .......... .......... .......... 22% 37.4M 23s
59600K .......... .......... .......... .......... .......... 22% 21.7M 23s
59650K .......... .......... .......... .......... .......... 22% 23.6M 23s
59700K .......... .......... .......... .......... .......... 22% 26.3M 23s
59750K .......... .......... .......... .......... .......... 22% 12.4M 23s
59800K .......... .......... .......... .......... .......... 22% 124M 23s
59850K .......... .......... .......... .......... .......... 22% 17.9M 23s
59900K .......... .......... .......... .......... .......... 22% 15.8M 23s
59950K .......... .......... .......... .......... .......... 22% 9.40M 23s
60000K .......... .......... .......... .......... .......... 22% 7.39M 23s
60050K .......... .......... .......... .......... .......... 22% 8.82M 23s
60100K .......... .......... .......... .......... .......... 22% 7.30M 23s
60150K .......... .......... .......... .......... .......... 22% 8.70M 23s
60200K .......... .......... .......... .......... .......... 22% 11.3M 23s
60250K .......... .......... .......... .......... .......... 22% 11.7M 23s
60300K .......... .......... .......... .......... .......... 22% 8.70M 23s
60350K .......... .......... .......... .......... .......... 22% 7.54M 23s
60400K .......... .......... .......... .......... .......... 22% 9.09M 23s
60450K .......... .......... .......... .......... .......... 22% 10.2M 23s
60500K .......... .......... .......... .......... .......... 22% 11.1M 23s
60550K .......... .......... .......... .......... .......... 22% 15.6M 23s
60600K .......... .......... .......... .......... .......... 22% 9.94M 23s
60650K .......... .......... .......... .......... .......... 22% 13.0M 23s
60700K .......... .......... .......... .......... .......... 22% 8.90M 23s
60750K .......... .......... .......... .......... .......... 22% 12.5M 23s
60800K .......... .......... .......... .......... .......... 22% 9.44M 23s
60850K .......... .......... .......... .......... .......... 22% 6.71M 23s
60900K .......... .......... .......... .......... .......... 22% 12.3M 23s
60950K .......... .......... .......... .......... .......... 22% 13.3M 23s
61000K .......... .......... .......... .......... .......... 22% 13.4M 23s
61050K .......... .......... .......... .......... .......... 22% 12.9M 23s
61100K .......... .......... .......... .......... .......... 23% 12.0M 23s
61150K .......... .......... .......... .......... .......... 23% 11.0M 23s
61200K .......... .......... .......... .......... .......... 23% 7.51M 23s
61250K .......... .......... .......... .......... .......... 23% 9.21M 23s
61300K .......... .......... .......... .......... .......... 23% 13.6M 23s
61350K .......... .......... .......... .......... .......... 23% 8.70M 23s
61400K .......... .......... .......... .......... .......... 23% 7.91M 23s
61450K .......... .......... .......... .......... .......... 23% 7.51M 23s
61500K .......... .......... .......... .......... .......... 23% 8.80M 23s
61550K .......... .......... .......... .......... .......... 23% 9.34M 23s
61600K .......... .......... .......... .......... .......... 23% 6.89M 23s
61650K .......... .......... .......... .......... .......... 23% 9.47M 23s
61700K .......... .......... .......... .......... .......... 23% 7.16M 23s
61750K .......... .......... .......... .......... .......... 23% 8.23M 23s
61800K .......... .......... .......... .......... .......... 23% 7.58M 23s
61850K .......... .......... .......... .......... .......... 23% 6.53M 23s
61900K .......... .......... .......... .......... .......... 23% 5.65M 23s
61950K .......... .......... .......... .......... .......... 23% 5.34M 23s
62000K .......... .......... .......... .......... .......... 23% 6.86M 23s
62050K .......... .......... .......... .......... .......... 23% 7.86M 23s
62100K .......... .......... .......... .......... .......... 23% 6.06M 23s
62150K .......... .......... .......... .......... .......... 23% 4.46M 23s
62200K .......... .......... .......... .......... .......... 23% 2.67M 23s
62250K .......... .......... .......... .......... .......... 23% 4.22M 23s
62300K .......... .......... .......... .......... .......... 23% 23.7M 23s
62350K .......... .......... .......... .......... .......... 23% 17.1M 23s
62400K .......... .......... .......... .......... .......... 23% 31.1M 23s
62450K .......... .......... .......... .......... .......... 23% 12.6M 23s
62500K .......... .......... .......... .......... .......... 23% 15.3M 23s
62550K .......... .......... .......... .......... .......... 23% 13.6M 23s
62600K .......... .......... .......... .......... .......... 23% 7.69M 23s
62650K .......... .......... .......... .......... .......... 23% 11.5M 23s
62700K .......... .......... .......... .......... .......... 23% 5.91M 23s
62750K .......... .......... .......... .......... .......... 23% 7.33M 23s
62800K .......... .......... .......... .......... .......... 23% 8.05M 23s
62850K .......... .......... .......... .......... .......... 23% 6.98M 23s
62900K .......... .......... .......... .......... .......... 23% 9.03M 23s
62950K .......... .......... .......... .......... .......... 23% 8.33M 23s
63000K .......... .......... .......... .......... .......... 23% 7.10M 23s
63050K .......... .......... .......... .......... .......... 23% 7.95M 23s
63100K .......... .......... .......... .......... .......... 23% 6.80M 23s
63150K .......... .......... .......... .......... .......... 23% 7.74M 23s
63200K .......... .......... .......... .......... .......... 23% 8.38M 23s
63250K .......... .......... .......... .......... .......... 23% 8.90M 23s
63300K .......... .......... .......... .......... .......... 23% 8.19M 23s
63350K .......... .......... .......... .......... .......... 23% 4.73M 23s
63400K .......... .......... .......... .......... .......... 23% 7.70M 23s
63450K .......... .......... .......... .......... .......... 23% 5.05M 23s
63500K .......... .......... .......... .......... .......... 23% 10.6M 23s
63550K .......... .......... .......... .......... .......... 23% 12.7M 23s
63600K .......... .......... .......... .......... .......... 23% 9.33M 23s
63650K .......... .......... .......... .......... .......... 23% 10.2M 23s
63700K .......... .......... .......... .......... .......... 23% 9.53M 23s
63750K .......... .......... .......... .......... .......... 24% 10.5M 23s
63800K .......... .......... .......... .......... .......... 24% 12.2M 23s
63850K .......... .......... .......... .......... .......... 24% 16.2M 23s
63900K .......... .......... .......... .......... .......... 24% 26.7M 23s
63950K .......... .......... .......... .......... .......... 24% 45.4M 23s
64000K .......... .......... .......... .......... .......... 24% 46.9M 23s
64050K .......... .......... .......... .......... .......... 24% 20.4M 23s
64100K .......... .......... .......... .......... .......... 24% 20.0M 22s
64150K .......... .......... .......... .......... .......... 24% 29.4M 22s
64200K .......... .......... .......... .......... .......... 24% 24.6M 22s
64250K .......... .......... .......... .......... .......... 24% 25.7M 22s
64300K .......... .......... .......... .......... .......... 24% 73.5M 22s
64350K .......... .......... .......... .......... .......... 24% 20.3M 22s
64400K .......... .......... .......... .......... .......... 24% 26.6M 22s
64450K .......... .......... .......... .......... .......... 24% 9.90M 22s
64500K .......... .......... .......... .......... .......... 24% 64.5M 22s
64550K .......... .......... .......... .......... .......... 24% 54.2M 22s
64600K .......... .......... .......... .......... .......... 24% 18.1M 22s
64650K .......... .......... .......... .......... .......... 24% 8.56M 22s
64700K .......... .......... .......... .......... .......... 24% 32.4M 22s
64750K .......... .......... .......... .......... .......... 24% 11.7M 22s
64800K .......... .......... .......... .......... .......... 24% 15.6M 22s
64850K .......... .......... .......... .......... .......... 24% 10.8M 22s
64900K .......... .......... .......... .......... .......... 24% 12.8M 22s
64950K .......... .......... .......... .......... .......... 24% 10.0M 22s
65000K .......... .......... .......... .......... .......... 24% 9.08M 22s
65050K .......... .......... .......... .......... .......... 24% 9.00M 22s
65100K .......... .......... .......... .......... .......... 24% 8.11M 22s
65150K .......... .......... .......... .......... .......... 24% 9.37M 22s
65200K .......... .......... .......... .......... .......... 24% 5.02M 22s
65250K .......... .......... .......... .......... .......... 24% 7.39M 22s
65300K .......... .......... .......... .......... .......... 24% 5.60M 22s
65350K .......... .......... .......... .......... .......... 24% 5.29M 22s
65400K .......... .......... .......... .......... .......... 24% 6.75M 22s
65450K .......... .......... .......... .......... .......... 24% 4.77M 22s
65500K .......... .......... .......... .......... .......... 24% 5.73M 22s
65550K .......... .......... .......... .......... .......... 24% 6.52M 22s
65600K .......... .......... .......... .......... .......... 24% 5.44M 22s
65650K .......... .......... .......... .......... .......... 24% 7.20M 22s
65700K .......... .......... .......... .......... .......... 24% 6.69M 22s
65750K .......... .......... .......... .......... .......... 24% 10.6M 22s
65800K .......... .......... .......... .......... .......... 24% 20.4M 22s
65850K .......... .......... .......... .......... .......... 24% 29.6M 22s
65900K .......... .......... .......... .......... .......... 24% 9.45M 22s
65950K .......... .......... .......... .......... .......... 24% 8.17M 22s
66000K .......... .......... .......... .......... .......... 24% 7.52M 22s
66050K .......... .......... .......... .......... .......... 24% 5.34M 22s
66100K .......... .......... .......... .......... .......... 24% 4.34M 22s
66150K .......... .......... .......... .......... .......... 24% 5.54M 22s
66200K .......... .......... .......... .......... .......... 24% 9.83M 22s
66250K .......... .......... .......... .......... .......... 24% 7.14M 22s
66300K .......... .......... .......... .......... .......... 24% 10.6M 22s
66350K .......... .......... .......... .......... .......... 24% 8.73M 22s
66400K .......... .......... .......... .......... .......... 25% 14.0M 22s
66450K .......... .......... .......... .......... .......... 25% 7.60M 22s
66500K .......... .......... .......... .......... .......... 25% 8.67M 22s
66550K .......... .......... .......... .......... .......... 25% 14.8M 22s
66600K .......... .......... .......... .......... .......... 25% 10.7M 22s
66650K .......... .......... .......... .......... .......... 25% 10.2M 22s
66700K .......... .......... .......... .......... .......... 25% 13.4M 22s
66750K .......... .......... .......... .......... .......... 25% 13.4M 22s
66800K .......... .......... .......... .......... .......... 25% 9.59M 22s
66850K .......... .......... .......... .......... .......... 25% 11.4M 22s
66900K .......... .......... .......... .......... .......... 25% 11.6M 22s
66950K .......... .......... .......... .......... .......... 25% 12.5M 22s
67000K .......... .......... .......... .......... .......... 25% 12.6M 22s
67050K .......... .......... .......... .......... .......... 25% 10.3M 22s
67100K .......... .......... .......... .......... .......... 25% 14.2M 22s
67150K .......... .......... .......... .......... .......... 25% 6.51M 22s
67200K .......... .......... .......... .......... .......... 25% 16.6M 22s
67250K .......... .......... .......... .......... .......... 25% 8.15M 22s
67300K .......... .......... .......... .......... .......... 25% 6.05M 22s
67350K .......... .......... .......... .......... .......... 25% 7.64M 22s
67400K .......... .......... .......... .......... .......... 25% 6.37M 22s
67450K .......... .......... .......... .......... .......... 25% 6.83M 22s
67500K .......... .......... .......... .......... .......... 25% 5.22M 22s
67550K .......... .......... .......... .......... .......... 25% 6.98M 22s
67600K .......... .......... .......... .......... .......... 25% 4.78M 22s
67650K .......... .......... .......... .......... .......... 25% 4.83M 22s
67700K .......... .......... .......... .......... .......... 25% 5.35M 22s
67750K .......... .......... .......... .......... .......... 25% 4.29M 22s
67800K .......... .......... .......... .......... .......... 25% 4.91M 22s
67850K .......... .......... .......... .......... .......... 25% 5.37M 22s
67900K .......... .......... .......... .......... .......... 25% 7.37M 22s
67950K .......... .......... .......... .......... .......... 25% 5.21M 22s
68000K .......... .......... .......... .......... .......... 25% 6.37M 22s
68050K .......... .......... .......... .......... .......... 25% 7.87M 22s
68100K .......... .......... .......... .......... .......... 25% 5.13M 22s
68150K .......... .......... .......... .......... .......... 25% 6.15M 22s
68200K .......... .......... .......... .......... .......... 25% 7.80M 22s
68250K .......... .......... .......... .......... .......... 25% 10.2M 22s
68300K .......... .......... .......... .......... .......... 25% 10.0M 22s
68350K .......... .......... .......... .......... .......... 25% 8.69M 22s
68400K .......... .......... .......... .......... .......... 25% 9.29M 22s
68450K .......... .......... .......... .......... .......... 25% 9.36M 22s
68500K .......... .......... .......... .......... .......... 25% 12.1M 22s
68550K .......... .......... .......... .......... .......... 25% 9.38M 22s
68600K .......... .......... .......... .......... .......... 25% 5.29M 22s
68650K .......... .......... .......... .......... .......... 25% 8.04M 22s
68700K .......... .......... .......... .......... .......... 25% 16.2M 22s
68750K .......... .......... .......... .......... .......... 25% 22.1M 22s
68800K .......... .......... .......... .......... .......... 25% 17.1M 22s
68850K .......... .......... .......... .......... .......... 25% 17.1M 22s
68900K .......... .......... .......... .......... .......... 25% 21.0M 22s
68950K .......... .......... .......... .......... .......... 25% 15.1M 22s
69000K .......... .......... .......... .......... .......... 25% 16.1M 22s
69050K .......... .......... .......... .......... .......... 25% 14.4M 22s
69100K .......... .......... .......... .......... .......... 26% 12.0M 22s
69150K .......... .......... .......... .......... .......... 26% 11.5M 22s
69200K .......... .......... .......... .......... .......... 26% 9.13M 22s
69250K .......... .......... .......... .......... .......... 26% 6.53M 22s
69300K .......... .......... .......... .......... .......... 26% 3.35M 22s
69350K .......... .......... .......... .......... .......... 26% 31.1M 22s
69400K .......... .......... .......... .......... .......... 26% 7.06M 22s
69450K .......... .......... .......... .......... .......... 26% 9.46M 22s
69500K .......... .......... .......... .......... .......... 26% 14.4M 22s
69550K .......... .......... .......... .......... .......... 26% 8.16M 22s
69600K .......... .......... .......... .......... .......... 26% 11.7M 22s
69650K .......... .......... .......... .......... .......... 26% 17.7M 22s
69700K .......... .......... .......... .......... .......... 26% 10.6M 22s
69750K .......... .......... .......... .......... .......... 26% 11.7M 22s
69800K .......... .......... .......... .......... .......... 26% 14.4M 22s
69850K .......... .......... .......... .......... .......... 26% 12.5M 22s
69900K .......... .......... .......... .......... .......... 26% 11.9M 22s
69950K .......... .......... .......... .......... .......... 26% 10.7M 22s
70000K .......... .......... .......... .......... .......... 26% 15.4M 22s
70050K .......... .......... .......... .......... .......... 26% 14.2M 22s
70100K .......... .......... .......... .......... .......... 26% 12.9M 22s
70150K .......... .......... .......... .......... .......... 26% 15.0M 22s
70200K .......... .......... .......... .......... .......... 26% 12.2M 22s
70250K .......... .......... .......... .......... .......... 26% 11.4M 22s
70300K .......... .......... .......... .......... .......... 26% 12.8M 22s
70350K .......... .......... .......... .......... .......... 26% 12.8M 22s
70400K .......... .......... .......... .......... .......... 26% 14.4M 22s
70450K .......... .......... .......... .......... .......... 26% 12.6M 22s
70500K .......... .......... .......... .......... .......... 26% 15.8M 22s
70550K .......... .......... .......... .......... .......... 26% 14.0M 22s
70600K .......... .......... .......... .......... .......... 26% 9.65M 22s
70650K .......... .......... .......... .......... .......... 26% 11.8M 22s
70700K .......... .......... .......... .......... .......... 26% 6.82M 22s
70750K .......... .......... .......... .......... .......... 26% 7.40M 22s
70800K .......... .......... .......... .......... .......... 26% 7.02M 22s
70850K .......... .......... .......... .......... .......... 26% 7.48M 22s
70900K .......... .......... .......... .......... .......... 26% 8.10M 22s
70950K .......... .......... .......... .......... .......... 26% 10.1M 22s
71000K .......... .......... .......... .......... .......... 26% 10.5M 22s
71050K .......... .......... .......... .......... .......... 26% 10.7M 22s
71100K .......... .......... .......... .......... .......... 26% 12.8M 22s
71150K .......... .......... .......... .......... .......... 26% 12.8M 22s
71200K .......... .......... .......... .......... .......... 26% 9.17M 22s
71250K .......... .......... .......... .......... .......... 26% 12.5M 22s
71300K .......... .......... .......... .......... .......... 26% 9.25M 22s
71350K .......... .......... .......... .......... .......... 26% 8.07M 22s
71400K .......... .......... .......... .......... .......... 26% 9.75M 22s
71450K .......... .......... .......... .......... .......... 26% 8.27M 22s
71500K .......... .......... .......... .......... .......... 26% 9.07M 22s
71550K .......... .......... .......... .......... .......... 26% 7.31M 22s
71600K .......... .......... .......... .......... .......... 26% 6.17M 22s
71650K .......... .......... .......... .......... .......... 26% 10.0M 22s
71700K .......... .......... .......... .......... .......... 26% 8.45M 22s
71750K .......... .......... .......... .......... .......... 27% 9.00M 22s
71800K .......... .......... .......... .......... .......... 27% 9.29M 22s
71850K .......... .......... .......... .......... .......... 27% 7.81M 22s
71900K .......... .......... .......... .......... .......... 27% 9.50M 22s
71950K .......... .......... .......... .......... .......... 27% 8.71M 22s
72000K .......... .......... .......... .......... .......... 27% 23.7M 21s
72050K .......... .......... .......... .......... .......... 27% 22.0M 21s
72100K .......... .......... .......... .......... .......... 27% 13.0M 21s
72150K .......... .......... .......... .......... .......... 27% 29.5M 21s
72200K .......... .......... .......... .......... .......... 27% 14.5M 21s
72250K .......... .......... .......... .......... .......... 27% 29.5M 21s
72300K .......... .......... .......... .......... .......... 27% 22.2M 21s
72350K .......... .......... .......... .......... .......... 27% 16.0M 21s
72400K .......... .......... .......... .......... .......... 27% 18.0M 21s
72450K .......... .......... .......... .......... .......... 27% 12.0M 21s
72500K .......... .......... .......... .......... .......... 27% 9.95M 21s
72550K .......... .......... .......... .......... .......... 27% 9.17M 21s
72600K .......... .......... .......... .......... .......... 27% 8.29M 21s
72650K .......... .......... .......... .......... .......... 27% 10.1M 21s
72700K .......... .......... .......... .......... .......... 27% 6.77M 21s
72750K .......... .......... .......... .......... .......... 27% 9.16M 21s
72800K .......... .......... .......... .......... .......... 27% 9.25M 21s
72850K .......... .......... .......... .......... .......... 27% 6.44M 21s
72900K .......... .......... .......... .......... .......... 27% 6.57M 21s
72950K .......... .......... .......... .......... .......... 27% 8.16M 21s
73000K .......... .......... .......... .......... .......... 27% 7.60M 21s
73050K .......... .......... .......... .......... .......... 27% 7.00M 21s
73100K .......... .......... .......... .......... .......... 27% 9.87M 21s
73150K .......... .......... .......... .......... .......... 27% 13.0M 21s
73200K .......... .......... .......... .......... .......... 27% 14.7M 21s
73250K .......... .......... .......... .......... .......... 27% 34.8M 21s
73300K .......... .......... .......... .......... .......... 27% 27.5M 21s
73350K .......... .......... .......... .......... .......... 27% 29.5M 21s
73400K .......... .......... .......... .......... .......... 27% 18.6M 21s
73450K .......... .......... .......... .......... .......... 27% 19.7M 21s
73500K .......... .......... .......... .......... .......... 27% 16.2M 21s
73550K .......... .......... .......... .......... .......... 27% 26.3M 21s
73600K .......... .......... .......... .......... .......... 27% 14.4M 21s
73650K .......... .......... .......... .......... .......... 27% 15.8M 21s
73700K .......... .......... .......... .......... .......... 27% 17.0M 21s
73750K .......... .......... .......... .......... .......... 27% 18.3M 21s
73800K .......... .......... .......... .......... .......... 27% 23.5M 21s
73850K .......... .......... .......... .......... .......... 27% 13.7M 21s
73900K .......... .......... .......... .......... .......... 27% 19.3M 21s
73950K .......... .......... .......... .......... .......... 27% 11.2M 21s
74000K .......... .......... .......... .......... .......... 27% 18.6M 21s
74050K .......... .......... .......... .......... .......... 27% 12.6M 21s
74100K .......... .......... .......... .......... .......... 27% 11.5M 21s
74150K .......... .......... .......... .......... .......... 27% 9.17M 21s
74200K .......... .......... .......... .......... .......... 27% 9.95M 21s
74250K .......... .......... .......... .......... .......... 27% 14.0M 21s
74300K .......... .......... .......... .......... .......... 27% 10.9M 21s
74350K .......... .......... .......... .......... .......... 27% 9.25M 21s
74400K .......... .......... .......... .......... .......... 28% 11.1M 21s
74450K .......... .......... .......... .......... .......... 28% 8.27M 21s
74500K .......... .......... .......... .......... .......... 28% 7.95M 21s
74550K .......... .......... .......... .......... .......... 28% 6.19M 21s
74600K .......... .......... .......... .......... .......... 28% 6.83M 21s
74650K .......... .......... .......... .......... .......... 28% 6.27M 21s
74700K .......... .......... .......... .......... .......... 28% 5.05M 21s
74750K .......... .......... .......... .......... .......... 28% 5.02M 21s
74800K .......... .......... .......... .......... .......... 28% 6.03M 21s
74850K .......... .......... .......... .......... .......... 28% 3.06M 21s
74900K .......... .......... .......... .......... .......... 28% 4.76M 21s
74950K .......... .......... .......... .......... .......... 28% 7.07M 21s
75000K .......... .......... .......... .......... .......... 28% 15.9M 21s
75050K .......... .......... .......... .......... .......... 28% 8.98M 21s
75100K .......... .......... .......... .......... .......... 28% 7.43M 21s
75150K .......... .......... .......... .......... .......... 28% 9.69M 21s
75200K .......... .......... .......... .......... .......... 28% 7.19M 21s
75250K .......... .......... .......... .......... .......... 28% 8.48M 21s
75300K .......... .......... .......... .......... .......... 28% 8.33M 21s
75350K .......... .......... .......... .......... .......... 28% 8.83M 21s
75400K .......... .......... .......... .......... .......... 28% 8.70M 21s
75450K .......... .......... .......... .......... .......... 28% 11.6M 21s
75500K .......... .......... .......... .......... .......... 28% 9.41M 21s
75550K .......... .......... .......... .......... .......... 28% 10.1M 21s
75600K .......... .......... .......... .......... .......... 28% 8.88M 21s
75650K .......... .......... .......... .......... .......... 28% 11.3M 21s
75700K .......... .......... .......... .......... .......... 28% 13.6M 21s
75750K .......... .......... .......... .......... .......... 28% 8.44M 21s
75800K .......... .......... .......... .......... .......... 28% 11.3M 21s
75850K .......... .......... .......... .......... .......... 28% 10.2M 21s
75900K .......... .......... .......... .......... .......... 28% 10.7M 21s
75950K .......... .......... .......... .......... .......... 28% 6.87M 21s
76000K .......... .......... .......... .......... .......... 28% 10.7M 21s
76050K .......... .......... .......... .......... .......... 28% 8.54M 21s
76100K .......... .......... .......... .......... .......... 28% 8.46M 21s
76150K .......... .......... .......... .......... .......... 28% 15.1M 21s
76200K .......... .......... .......... .......... .......... 28% 9.72M 21s
76250K .......... .......... .......... .......... .......... 28% 18.7M 21s
76300K .......... .......... .......... .......... .......... 28% 12.3M 21s
76350K .......... .......... .......... .......... .......... 28% 13.1M 21s
76400K .......... .......... .......... .......... .......... 28% 15.2M 21s
76450K .......... .......... .......... .......... .......... 28% 16.5M 21s
76500K .......... .......... .......... .......... .......... 28% 22.2M 21s
76550K .......... .......... .......... .......... .......... 28% 29.6M 21s
76600K .......... .......... .......... .......... .......... 28% 18.3M 21s
76650K .......... .......... .......... .......... .......... 28% 35.1M 21s
76700K .......... .......... .......... .......... .......... 28% 19.3M 21s
76750K .......... .......... .......... .......... .......... 28% 27.6M 21s
76800K .......... .......... .......... .......... .......... 28% 17.6M 21s
76850K .......... .......... .......... .......... .......... 28% 14.3M 21s
76900K .......... .......... .......... .......... .......... 28% 23.5M 21s
76950K .......... .......... .......... .......... .......... 28% 14.6M 21s
77000K .......... .......... .......... .......... .......... 28% 22.3M 21s
77050K .......... .......... .......... .......... .......... 29% 19.8M 21s
77100K .......... .......... .......... .......... .......... 29% 17.0M 21s
77150K .......... .......... .......... .......... .......... 29% 19.3M 21s
77200K .......... .......... .......... .......... .......... 29% 22.8M 21s
77250K .......... .......... .......... .......... .......... 29% 22.5M 21s
77300K .......... .......... .......... .......... .......... 29% 19.3M 21s
77350K .......... .......... .......... .......... .......... 29% 20.6M 21s
77400K .......... .......... .......... .......... .......... 29% 17.6M 21s
77450K .......... .......... .......... .......... .......... 29% 15.9M 21s
77500K .......... .......... .......... .......... .......... 29% 18.9M 21s
77550K .......... .......... .......... .......... .......... 29% 26.2M 21s
77600K .......... .......... .......... .......... .......... 29% 18.2M 21s
77650K .......... .......... .......... .......... .......... 29% 8.87M 21s
77700K .......... .......... .......... .......... .......... 29% 37.3M 21s
77750K .......... .......... .......... .......... .......... 29% 13.8M 21s
77800K .......... .......... .......... .......... .......... 29% 21.2M 21s
77850K .......... .......... .......... .......... .......... 29% 8.28M 20s
77900K .......... .......... .......... .......... .......... 29% 14.8M 20s
77950K .......... .......... .......... .......... .......... 29% 8.01M 20s
78000K .......... .......... .......... .......... .......... 29% 13.3M 20s
78050K .......... .......... .......... .......... .......... 29% 16.9M 20s
78100K .......... .......... .......... .......... .......... 29% 11.4M 20s
78150K .......... .......... .......... .......... .......... 29% 10.6M 20s
78200K .......... .......... .......... .......... .......... 29% 14.6M 20s
78250K .......... .......... .......... .......... .......... 29% 11.0M 20s
78300K .......... .......... .......... .......... .......... 29% 7.09M 20s
78350K .......... .......... .......... .......... .......... 29% 38.0M 20s
78400K .......... .......... .......... .......... .......... 29% 9.67M 20s
78450K .......... .......... .......... .......... .......... 29% 13.0M 20s
78500K .......... .......... .......... .......... .......... 29% 13.2M 20s
78550K .......... .......... .......... .......... .......... 29% 15.4M 20s
78600K .......... .......... .......... .......... .......... 29% 10.4M 20s
78650K .......... .......... .......... .......... .......... 29% 17.6M 20s
78700K .......... .......... .......... .......... .......... 29% 10.7M 20s
78750K .......... .......... .......... .......... .......... 29% 11.2M 20s
78800K .......... .......... .......... .......... .......... 29% 11.0M 20s
78850K .......... .......... .......... .......... .......... 29% 9.97M 20s
78900K .......... .......... .......... .......... .......... 29% 13.4M 20s
78950K .......... .......... .......... .......... .......... 29% 10.4M 20s
79000K .......... .......... .......... .......... .......... 29% 7.00M 20s
79050K .......... .......... .......... .......... .......... 29% 9.07M 20s
79100K .......... .......... .......... .......... .......... 29% 7.32M 20s
79150K .......... .......... .......... .......... .......... 29% 10.2M 20s
79200K .......... .......... .......... .......... .......... 29% 20.9M 20s
79250K .......... .......... .......... .......... .......... 29% 14.6M 20s
79300K .......... .......... .......... .......... .......... 29% 10.3M 20s
79350K .......... .......... .......... .......... .......... 29% 7.49M 20s
79400K .......... .......... .......... .......... .......... 29% 7.25M 20s
79450K .......... .......... .......... .......... .......... 29% 7.10M 20s
79500K .......... .......... .......... .......... .......... 29% 8.15M 20s
79550K .......... .......... .......... .......... .......... 29% 8.63M 20s
79600K .......... .......... .......... .......... .......... 29% 7.35M 20s
79650K .......... .......... .......... .......... .......... 29% 10.8M 20s
79700K .......... .......... .......... .......... .......... 30% 12.1M 20s
79750K .......... .......... .......... .......... .......... 30% 10.1M 20s
79800K .......... .......... .......... .......... .......... 30% 14.3M 20s
79850K .......... .......... .......... .......... .......... 30% 9.66M 20s
79900K .......... .......... .......... .......... .......... 30% 7.63M 20s
79950K .......... .......... .......... .......... .......... 30% 3.73M 20s
80000K .......... .......... .......... .......... .......... 30% 7.62M 20s
80050K .......... .......... .......... .......... .......... 30% 6.20M 20s
80100K .......... .......... .......... .......... .......... 30% 7.47M 20s
80150K .......... .......... .......... .......... .......... 30% 28.9M 20s
80200K .......... .......... .......... .......... .......... 30% 11.0M 20s
80250K .......... .......... .......... .......... .......... 30% 8.71M 20s
80300K .......... .......... .......... .......... .......... 30% 21.4M 20s
80350K .......... .......... .......... .......... .......... 30% 10.4M 20s
80400K .......... .......... .......... .......... .......... 30% 10.1M 20s
80450K .......... .......... .......... .......... .......... 30% 6.65M 20s
80500K .......... .......... .......... .......... .......... 30% 8.03M 20s
80550K .......... .......... .......... .......... .......... 30% 7.99M 20s
80600K .......... .......... .......... .......... .......... 30% 6.04M 20s
80650K .......... .......... .......... .......... .......... 30% 6.37M 20s
80700K .......... .......... .......... .......... .......... 30% 7.38M 20s
80750K .......... .......... .......... .......... .......... 30% 7.46M 20s
80800K .......... .......... .......... .......... .......... 30% 7.28M 20s
80850K .......... .......... .......... .......... .......... 30% 10.2M 20s
80900K .......... .......... .......... .......... .......... 30% 9.08M 20s
80950K .......... .......... .......... .......... .......... 30% 7.20M 20s
81000K .......... .......... .......... .......... .......... 30% 7.34M 20s
81050K .......... .......... .......... .......... .......... 30% 4.99M 20s
81100K .......... .......... .......... .......... .......... 30% 4.60M 20s
81150K .......... .......... .......... .......... .......... 30% 3.92M 20s
81200K .......... .......... .......... .......... .......... 30% 17.6M 20s
81250K .......... .......... .......... .......... .......... 30% 16.5M 20s
81300K .......... .......... .......... .......... .......... 30% 25.6M 20s
81350K .......... .......... .......... .......... .......... 30% 23.7M 20s
81400K .......... .......... .......... .......... .......... 30% 54.2M 20s
81450K .......... .......... .......... .......... .......... 30% 12.6M 20s
81500K .......... .......... .......... .......... .......... 30% 23.0M 20s
81550K .......... .......... .......... .......... .......... 30% 8.21M 20s
81600K .......... .......... .......... .......... .......... 30% 7.48M 20s
81650K .......... .......... .......... .......... .......... 30% 7.69M 20s
81700K .......... .......... .......... .......... .......... 30% 8.00M 20s
81750K .......... .......... .......... .......... .......... 30% 6.78M 20s
81800K .......... .......... .......... .......... .......... 30% 7.79M 20s
81850K .......... .......... .......... .......... .......... 30% 9.16M 20s
81900K .......... .......... .......... .......... .......... 30% 7.92M 20s
81950K .......... .......... .......... .......... .......... 30% 6.35M 20s
82000K .......... .......... .......... .......... .......... 30% 6.77M 20s
82050K .......... .......... .......... .......... .......... 30% 3.66M 20s
82100K .......... .......... .......... .......... .......... 30% 4.92M 20s
82150K .......... .......... .......... .......... .......... 30% 14.1M 20s
82200K .......... .......... .......... .......... .......... 30% 7.69M 20s
82250K .......... .......... .......... .......... .......... 30% 182M 20s
82300K .......... .......... .......... .......... .......... 30% 11.1M 20s
82350K .......... .......... .......... .......... .......... 31% 10.5M 20s
82400K .......... .......... .......... .......... .......... 31% 19.4M 20s
82450K .......... .......... .......... .......... .......... 31% 11.3M 20s
82500K .......... .......... .......... .......... .......... 31% 13.7M 20s
82550K .......... .......... .......... .......... .......... 31% 14.7M 20s
82600K .......... .......... .......... .......... .......... 31% 15.4M 20s
82650K .......... .......... .......... .......... .......... 31% 13.9M 20s
82700K .......... .......... .......... .......... .......... 31% 21.1M 20s
82750K .......... .......... .......... .......... .......... 31% 13.4M 20s
82800K .......... .......... .......... .......... .......... 31% 20.8M 20s
82850K .......... .......... .......... .......... .......... 31% 24.3M 20s
82900K .......... .......... .......... .......... .......... 31% 21.9M 20s
82950K .......... .......... .......... .......... .......... 31% 13.3M 20s
83000K .......... .......... .......... .......... .......... 31% 33.6M 20s
83050K .......... .......... .......... .......... .......... 31% 18.9M 20s
83100K .......... .......... .......... .......... .......... 31% 22.0M 20s
83150K .......... .......... .......... .......... .......... 31% 13.3M 20s
83200K .......... .......... .......... .......... .......... 31% 17.2M 20s
83250K .......... .......... .......... .......... .......... 31% 18.8M 20s
83300K .......... .......... .......... .......... .......... 31% 17.1M 20s
83350K .......... .......... .......... .......... .......... 31% 12.4M 20s
83400K .......... .......... .......... .......... .......... 31% 11.7M 20s
83450K .......... .......... .......... .......... .......... 31% 9.49M 20s
83500K .......... .......... .......... .......... .......... 31% 8.60M 20s
83550K .......... .......... .......... .......... .......... 31% 9.04M 20s
83600K .......... .......... .......... .......... .......... 31% 11.6M 20s
83650K .......... .......... .......... .......... .......... 31% 16.3M 20s
83700K .......... .......... .......... .......... .......... 31% 19.7M 20s
83750K .......... .......... .......... .......... .......... 31% 25.9M 20s
83800K .......... .......... .......... .......... .......... 31% 15.9M 20s
83850K .......... .......... .......... .......... .......... 31% 10.1M 20s
83900K .......... .......... .......... .......... .......... 31% 32.1M 20s
83950K .......... .......... .......... .......... .......... 31% 10.7M 20s
84000K .......... .......... .......... .......... .......... 31% 17.4M 20s
84050K .......... .......... .......... .......... .......... 31% 13.2M 20s
84100K .......... .......... .......... .......... .......... 31% 10.9M 20s
84150K .......... .......... .......... .......... .......... 31% 11.8M 20s
84200K .......... .......... .......... .......... .......... 31% 10.6M 20s
84250K .......... .......... .......... .......... .......... 31% 13.3M 20s
84300K .......... .......... .......... .......... .......... 31% 8.57M 20s
84350K .......... .......... .......... .......... .......... 31% 23.4M 20s
84400K .......... .......... .......... .......... .......... 31% 13.6M 20s
84450K .......... .......... .......... .......... .......... 31% 10.7M 20s
84500K .......... .......... .......... .......... .......... 31% 16.2M 20s
84550K .......... .......... .......... .......... .......... 31% 11.5M 20s
84600K .......... .......... .......... .......... .......... 31% 11.5M 20s
84650K .......... .......... .......... .......... .......... 31% 11.7M 20s
84700K .......... .......... .......... .......... .......... 31% 13.0M 20s
84750K .......... .......... .......... .......... .......... 31% 14.8M 20s
84800K .......... .......... .......... .......... .......... 31% 13.7M 20s
84850K .......... .......... .......... .......... .......... 31% 10.3M 20s
84900K .......... .......... .......... .......... .......... 31% 12.1M 20s
84950K .......... .......... .......... .......... .......... 31% 11.0M 19s
85000K .......... .......... .......... .......... .......... 32% 9.90M 19s
85050K .......... .......... .......... .......... .......... 32% 11.4M 19s
85100K .......... .......... .......... .......... .......... 32% 8.61M 19s
85150K .......... .......... .......... .......... .......... 32% 10.7M 19s
85200K .......... .......... .......... .......... .......... 32% 7.75M 19s
85250K .......... .......... .......... .......... .......... 32% 10.7M 19s
85300K .......... .......... .......... .......... .......... 32% 8.91M 19s
85350K .......... .......... .......... .......... .......... 32% 6.37M 19s
85400K .......... .......... .......... .......... .......... 32% 7.15M 19s
85450K .......... .......... .......... .......... .......... 32% 5.98M 19s
85500K .......... .......... .......... .......... .......... 32% 9.77M 19s
85550K .......... .......... .......... .......... .......... 32% 15.6M 19s
85600K .......... .......... .......... .......... .......... 32% 16.7M 19s
85650K .......... .......... .......... .......... .......... 32% 22.8M 19s
85700K .......... .......... .......... .......... .......... 32% 14.2M 19s
85750K .......... .......... .......... .......... .......... 32% 30.5M 19s
85800K .......... .......... .......... .......... .......... 32% 17.5M 19s
85850K .......... .......... .......... .......... .......... 32% 15.6M 19s
85900K .......... .......... .......... .......... .......... 32% 14.8M 19s
85950K .......... .......... .......... .......... .......... 32% 10.4M 19s
86000K .......... .......... .......... .......... .......... 32% 19.0M 19s
86050K .......... .......... .......... .......... .......... 32% 10.1M 19s
86100K .......... .......... .......... .......... .......... 32% 9.54M 19s
86150K .......... .......... .......... .......... .......... 32% 10.2M 19s
86200K .......... .......... .......... .......... .......... 32% 9.55M 19s
86250K .......... .......... .......... .......... .......... 32% 13.1M 19s
86300K .......... .......... .......... .......... .......... 32% 13.0M 19s
86350K .......... .......... .......... .......... .......... 32% 10.7M 19s
86400K .......... .......... .......... .......... .......... 32% 11.3M 19s
86450K .......... .......... .......... .......... .......... 32% 9.14M 19s
86500K .......... .......... .......... .......... .......... 32% 9.97M 19s
86550K .......... .......... .......... .......... .......... 32% 9.29M 19s
86600K .......... .......... .......... .......... .......... 32% 11.5M 19s
86650K .......... .......... .......... .......... .......... 32% 10.2M 19s
86700K .......... .......... .......... .......... .......... 32% 6.59M 19s
86750K .......... .......... .......... .......... .......... 32% 7.36M 19s
86800K .......... .......... .......... .......... .......... 32% 8.94M 19s
86850K .......... .......... .......... .......... .......... 32% 6.59M 19s
86900K .......... .......... .......... .......... .......... 32% 8.67M 19s
86950K .......... .......... .......... .......... .......... 32% 7.49M 19s
87000K .......... .......... .......... .......... .......... 32% 11.2M 19s
87050K .......... .......... .......... .......... .......... 32% 10.3M 19s
87100K .......... .......... .......... .......... .......... 32% 13.0M 19s
87150K .......... .......... .......... .......... .......... 32% 10.1M 19s
87200K .......... .......... .......... .......... .......... 32% 8.83M 19s
87250K .......... .......... .......... .......... .......... 32% 8.15M 19s
87300K .......... .......... .......... .......... .......... 32% 8.00M 19s
87350K .......... .......... .......... .......... .......... 32% 5.73M 19s
87400K .......... .......... .......... .......... .......... 32% 7.53M 19s
87450K .......... .......... .......... .......... .......... 32% 9.87M 19s
87500K .......... .......... .......... .......... .......... 32% 8.28M 19s
87550K .......... .......... .......... .......... .......... 32% 10.9M 19s
87600K .......... .......... .......... .......... .......... 32% 8.72M 19s
87650K .......... .......... .......... .......... .......... 32% 10.4M 19s
87700K .......... .......... .......... .......... .......... 33% 8.08M 19s
87750K .......... .......... .......... .......... .......... 33% 9.53M 19s
87800K .......... .......... .......... .......... .......... 33% 9.67M 19s
87850K .......... .......... .......... .......... .......... 33% 4.73M 19s
87900K .......... .......... .......... .......... .......... 33% 5.84M 19s
87950K .......... .......... .......... .......... .......... 33% 6.12M 19s
88000K .......... .......... .......... .......... .......... 33% 6.58M 19s
88050K .......... .......... .......... .......... .......... 33% 13.6M 19s
88100K .......... .......... .......... .......... .......... 33% 11.0M 19s
88150K .......... .......... .......... .......... .......... 33% 8.35M 19s
88200K .......... .......... .......... .......... .......... 33% 11.8M 19s
88250K .......... .......... .......... .......... .......... 33% 12.3M 19s
88300K .......... .......... .......... .......... .......... 33% 9.35M 19s
88350K .......... .......... .......... .......... .......... 33% 9.12M 19s
88400K .......... .......... .......... .......... .......... 33% 9.95M 19s
88450K .......... .......... .......... .......... .......... 33% 9.32M 19s
88500K .......... .......... .......... .......... .......... 33% 12.5M 19s
88550K .......... .......... .......... .......... .......... 33% 10.3M 19s
88600K .......... .......... .......... .......... .......... 33% 11.5M 19s
88650K .......... .......... .......... .......... .......... 33% 38.9M 19s
88700K .......... .......... .......... .......... .......... 33% 23.1M 19s
88750K .......... .......... .......... .......... .......... 33% 12.5M 19s
88800K .......... .......... .......... .......... .......... 33% 70.3M 19s
88850K .......... .......... .......... .......... .......... 33% 27.3M 19s
88900K .......... .......... .......... .......... .......... 33% 72.8M 19s
88950K .......... .......... .......... .......... .......... 33% 59.2M 19s
89000K .......... .......... .......... .......... .......... 33% 22.2M 19s
89050K .......... .......... .......... .......... .......... 33% 60.3M 19s
89100K .......... .......... .......... .......... .......... 33% 26.8M 19s
89150K .......... .......... .......... .......... .......... 33% 22.7M 19s
89200K .......... .......... .......... .......... .......... 33% 25.2M 19s
89250K .......... .......... .......... .......... .......... 33% 8.55M 19s
89300K .......... .......... .......... .......... .......... 33% 73.6M 19s
89350K .......... .......... .......... .......... .......... 33% 12.0M 19s
89400K .......... .......... .......... .......... .......... 33% 13.9M 19s
89450K .......... .......... .......... .......... .......... 33% 12.1M 19s
89500K .......... .......... .......... .......... .......... 33% 13.9M 19s
89550K .......... .......... .......... .......... .......... 33% 12.9M 19s
89600K .......... .......... .......... .......... .......... 33% 10.1M 19s
89650K .......... .......... .......... .......... .......... 33% 13.9M 19s
89700K .......... .......... .......... .......... .......... 33% 11.1M 19s
89750K .......... .......... .......... .......... .......... 33% 11.8M 19s
89800K .......... .......... .......... .......... .......... 33% 13.5M 19s
89850K .......... .......... .......... .......... .......... 33% 19.4M 19s
89900K .......... .......... .......... .......... .......... 33% 9.34M 19s
89950K .......... .......... .......... .......... .......... 33% 14.2M 19s
90000K .......... .......... .......... .......... .......... 33% 15.0M 19s
90050K .......... .......... .......... .......... .......... 33% 14.3M 19s
90100K .......... .......... .......... .......... .......... 33% 12.6M 19s
90150K .......... .......... .......... .......... .......... 33% 11.7M 19s
90200K .......... .......... .......... .......... .......... 33% 10.7M 19s
90250K .......... .......... .......... .......... .......... 33% 9.07M 19s
90300K .......... .......... .......... .......... .......... 33% 9.60M 19s
90350K .......... .......... .......... .......... .......... 34% 7.73M 19s
90400K .......... .......... .......... .......... .......... 34% 10.5M 19s
90450K .......... .......... .......... .......... .......... 34% 7.89M 19s
90500K .......... .......... .......... .......... .......... 34% 8.95M 19s
90550K .......... .......... .......... .......... .......... 34% 10.4M 19s
90600K .......... .......... .......... .......... .......... 34% 9.57M 19s
90650K .......... .......... .......... .......... .......... 34% 16.2M 19s
90700K .......... .......... .......... .......... .......... 34% 14.7M 19s
90750K .......... .......... .......... .......... .......... 34% 19.6M 19s
90800K .......... .......... .......... .......... .......... 34% 13.7M 19s
90850K .......... .......... .......... .......... .......... 34% 7.54M 19s
90900K .......... .......... .......... .......... .......... 34% 10.3M 19s
90950K .......... .......... .......... .......... .......... 34% 10.3M 19s
91000K .......... .......... .......... .......... .......... 34% 9.64M 19s
91050K .......... .......... .......... .......... .......... 34% 10.3M 19s
91100K .......... .......... .......... .......... .......... 34% 11.0M 19s
91150K .......... .......... .......... .......... .......... 34% 9.42M 19s
91200K .......... .......... .......... .......... .......... 34% 5.90M 19s
91250K .......... .......... .......... .......... .......... 34% 6.82M 19s
91300K .......... .......... .......... .......... .......... 34% 8.51M 19s
91350K .......... .......... .......... .......... .......... 34% 6.88M 19s
91400K .......... .......... .......... .......... .......... 34% 5.63M 19s
91450K .......... .......... .......... .......... .......... 34% 5.91M 19s
91500K .......... .......... .......... .......... .......... 34% 9.50M 19s
91550K .......... .......... .......... .......... .......... 34% 14.2M 19s
91600K .......... .......... .......... .......... .......... 34% 11.8M 19s
91650K .......... .......... .......... .......... .......... 34% 10.8M 19s
91700K .......... .......... .......... .......... .......... 34% 7.85M 19s
91750K .......... .......... .......... .......... .......... 34% 9.30M 19s
91800K .......... .......... .......... .......... .......... 34% 8.94M 19s
91850K .......... .......... .......... .......... .......... 34% 5.83M 19s
91900K .......... .......... .......... .......... .......... 34% 7.40M 19s
91950K .......... .......... .......... .......... .......... 34% 4.37M 19s
92000K .......... .......... .......... .......... .......... 34% 7.77M 19s
92050K .......... .......... .......... .......... .......... 34% 28.1M 19s
92100K .......... .......... .......... .......... .......... 34% 6.89M 19s
92150K .......... .......... .......... .......... .......... 34% 5.97M 19s
92200K .......... .......... .......... .......... .......... 34% 4.36M 19s
92250K .......... .......... .......... .......... .......... 34% 4.66M 19s
92300K .......... .......... .......... .......... .......... 34% 5.36M 19s
92350K .......... .......... .......... .......... .......... 34% 13.4M 19s
92400K .......... .......... .......... .......... .......... 34% 9.11M 19s
92450K .......... .......... .......... .......... .......... 34% 4.05M 19s
92500K .......... .......... .......... .......... .......... 34% 21.7M 19s
92550K .......... .......... .......... .......... .......... 34% 10.2M 19s
92600K .......... .......... .......... .......... .......... 34% 3.88M 19s
92650K .......... .......... .......... .......... .......... 34% 66.9M 19s
92700K .......... .......... .......... .......... .......... 34% 4.49M 19s
92750K .......... .......... .......... .......... .......... 34% 187M 19s
92800K .......... .......... .......... .......... .......... 34% 11.9M 19s
92850K .......... .......... .......... .......... .......... 34% 8.17M 19s
92900K .......... .......... .......... .......... .......... 34% 4.53M 19s
92950K .......... .......... .......... .......... .......... 34% 83.5M 19s
93000K .......... .......... .......... .......... .......... 35% 11.0M 18s
93050K .......... .......... .......... .......... .......... 35% 10.6M 18s
93100K .......... .......... .......... .......... .......... 35% 5.55M 18s
93150K .......... .......... .......... .......... .......... 35% 10.2M 18s
93200K .......... .......... .......... .......... .......... 35% 5.81M 18s
93250K .......... .......... .......... .......... .......... 35% 5.93M 18s
93300K .......... .......... .......... .......... .......... 35% 6.41M 18s
93350K .......... .......... .......... .......... .......... 35% 5.50M 18s
93400K .......... .......... .......... .......... .......... 35% 9.22M 18s
93450K .......... .......... .......... .......... .......... 35% 6.48M 18s
93500K .......... .......... .......... .......... .......... 35% 7.53M 18s
93550K .......... .......... .......... .......... .......... 35% 7.49M 18s
93600K .......... .......... .......... .......... .......... 35% 3.88M 18s
93650K .......... .......... .......... .......... .......... 35% 279M 18s
93700K .......... .......... .......... .......... .......... 35% 6.36M 18s
93750K .......... .......... .......... .......... .......... 35% 8.23M 18s
93800K .......... .......... .......... .......... .......... 35% 11.4M 18s
93850K .......... .......... .......... .......... .......... 35% 13.2M 18s
93900K .......... .......... .......... .......... .......... 35% 17.7M 18s
93950K .......... .......... .......... .......... .......... 35% 49.2M 18s
94000K .......... .......... .......... .......... .......... 35% 14.5M 18s
94050K .......... .......... .......... .......... .......... 35% 27.6M 18s
94100K .......... .......... .......... .......... .......... 35% 11.5M 18s
94150K .......... .......... .......... .......... .......... 35% 10.0M 18s
94200K .......... .......... .......... .......... .......... 35% 9.73M 18s
94250K .......... .......... .......... .......... .......... 35% 17.0M 18s
94300K .......... .......... .......... .......... .......... 35% 12.2M 18s
94350K .......... .......... .......... .......... .......... 35% 11.5M 18s
94400K .......... .......... .......... .......... .......... 35% 14.9M 18s
94450K .......... .......... .......... .......... .......... 35% 11.0M 18s
94500K .......... .......... .......... .......... .......... 35% 13.7M 18s
94550K .......... .......... .......... .......... .......... 35% 12.3M 18s
94600K .......... .......... .......... .......... .......... 35% 13.5M 18s
94650K .......... .......... .......... .......... .......... 35% 94.7M 18s
94700K .......... .......... .......... .......... .......... 35% 28.1M 18s
94750K .......... .......... .......... .......... .......... 35% 126M 18s
94800K .......... .......... .......... .......... .......... 35% 28.1M 18s
94850K .......... .......... .......... .......... .......... 35% 25.9M 18s
94900K .......... .......... .......... .......... .......... 35% 29.1M 18s
94950K .......... .......... .......... .......... .......... 35% 42.7M 18s
95000K .......... .......... .......... .......... .......... 35% 21.3M 18s
95050K .......... .......... .......... .......... .......... 35% 27.3M 18s
95100K .......... .......... .......... .......... .......... 35% 9.76M 18s
95150K .......... .......... .......... .......... .......... 35% 24.2M 18s
95200K .......... .......... .......... .......... .......... 35% 59.0M 18s
95250K .......... .......... .......... .......... .......... 35% 9.49M 18s
95300K .......... .......... .......... .......... .......... 35% 273M 18s
95350K .......... .......... .......... .......... .......... 35% 22.8M 18s
95400K .......... .......... .......... .......... .......... 35% 20.2M 18s
95450K .......... .......... .......... .......... .......... 35% 11.4M 18s
95500K .......... .......... .......... .......... .......... 35% 16.6M 18s
95550K .......... .......... .......... .......... .......... 35% 20.5M 18s
95600K .......... .......... .......... .......... .......... 35% 17.3M 18s
95650K .......... .......... .......... .......... .......... 36% 7.83M 18s
95700K .......... .......... .......... .......... .......... 36% 54.3M 18s
95750K .......... .......... .......... .......... .......... 36% 16.7M 18s
95800K .......... .......... .......... .......... .......... 36% 5.35M 18s
95850K .......... .......... .......... .......... .......... 36% 8.37M 18s
95900K .......... .......... .......... .......... .......... 36% 11.4M 18s
95950K .......... .......... .......... .......... .......... 36% 8.86M 18s
96000K .......... .......... .......... .......... .......... 36% 18.9M 18s
96050K .......... .......... .......... .......... .......... 36% 13.8M 18s
96100K .......... .......... .......... .......... .......... 36% 10.0M 18s
96150K .......... .......... .......... .......... .......... 36% 8.12M 18s
96200K .......... .......... .......... .......... .......... 36% 5.41M 18s
96250K .......... .......... .......... .......... .......... 36% 9.86M 18s
96300K .......... .......... .......... .......... .......... 36% 12.2M 18s
96350K .......... .......... .......... .......... .......... 36% 12.2M 18s
96400K .......... .......... .......... .......... .......... 36% 11.0M 18s
96450K .......... .......... .......... .......... .......... 36% 7.68M 18s
96500K .......... .......... .......... .......... .......... 36% 11.2M 18s
96550K .......... .......... .......... .......... .......... 36% 9.72M 18s
96600K .......... .......... .......... .......... .......... 36% 7.10M 18s
96650K .......... .......... .......... .......... .......... 36% 12.6M 18s
96700K .......... .......... .......... .......... .......... 36% 19.6M 18s
96750K .......... .......... .......... .......... .......... 36% 13.3M 18s
96800K .......... .......... .......... .......... .......... 36% 12.3M 18s
96850K .......... .......... .......... .......... .......... 36% 15.5M 18s
96900K .......... .......... .......... .......... .......... 36% 15.8M 18s
96950K .......... .......... .......... .......... .......... 36% 12.8M 18s
97000K .......... .......... .......... .......... .......... 36% 8.66M 18s
97050K .......... .......... .......... .......... .......... 36% 6.61M 18s
97100K .......... .......... .......... .......... .......... 36% 6.42M 18s
97150K .......... .......... .......... .......... .......... 36% 6.73M 18s
97200K .......... .......... .......... .......... .......... 36% 7.27M 18s
97250K .......... .......... .......... .......... .......... 36% 11.7M 18s
97300K .......... .......... .......... .......... .......... 36% 11.5M 18s
97350K .......... .......... .......... .......... .......... 36% 8.75M 18s
97400K .......... .......... .......... .......... .......... 36% 9.26M 18s
97450K .......... .......... .......... .......... .......... 36% 7.90M 18s
97500K .......... .......... .......... .......... .......... 36% 6.99M 18s
97550K .......... .......... .......... .......... .......... 36% 46.1M 18s
97600K .......... .......... .......... .......... .......... 36% 7.96M 18s
97650K .......... .......... .......... .......... .......... 36% 109M 18s
97700K .......... .......... .......... .......... .......... 36% 4.65M 18s
97750K .......... .......... .......... .......... .......... 36% 59.8M 18s
97800K .......... .......... .......... .......... .......... 36% 12.6M 18s
97850K .......... .......... .......... .......... .......... 36% 8.09M 18s
97900K .......... .......... .......... .......... .......... 36% 11.7M 18s
97950K .......... .......... .......... .......... .......... 36% 8.14M 18s
98000K .......... .......... .......... .......... .......... 36% 15.2M 18s
98050K .......... .......... .......... .......... .......... 36% 11.7M 18s
98100K .......... .......... .......... .......... .......... 36% 19.4M 18s
98150K .......... .......... .......... .......... .......... 36% 39.0M 18s
98200K .......... .......... .......... .......... .......... 36% 17.4M 18s
98250K .......... .......... .......... .......... .......... 36% 141M 18s
98300K .......... .......... .......... .......... .......... 37% 16.4M 18s
98350K .......... .......... .......... .......... .......... 37% 18.7M 18s
98400K .......... .......... .......... .......... .......... 37% 16.8M 18s
98450K .......... .......... .......... .......... .......... 37% 11.1M 18s
98500K .......... .......... .......... .......... .......... 37% 16.1M 18s
98550K .......... .......... .......... .......... .......... 37% 8.90M 18s
98600K .......... .......... .......... .......... .......... 37% 11.8M 18s
98650K .......... .......... .......... .......... .......... 37% 9.30M 18s
98700K .......... .......... .......... .......... .......... 37% 6.15M 18s
98750K .......... .......... .......... .......... .......... 37% 110M 18s
98800K .......... .......... .......... .......... .......... 37% 9.02M 18s
98850K .......... .......... .......... .......... .......... 37% 4.65M 18s
98900K .......... .......... .......... .......... .......... 37% 16.9M 18s
98950K .......... .......... .......... .......... .......... 37% 4.02M 18s
99000K .......... .......... .......... .......... .......... 37% 2.05M 18s
99050K .......... .......... .......... .......... .......... 37% 153M 18s
99100K .......... .......... .......... .......... .......... 37% 58.9M 18s
99150K .......... .......... .......... .......... .......... 37% 56.7M 18s
99200K .......... .......... .......... .......... .......... 37% 13.9M 18s
99250K .......... .......... .......... .......... .......... 37% 4.59M 18s
99300K .......... .......... .......... .......... .......... 37% 5.59M 18s
99350K .......... .......... .......... .......... .......... 37% 5.47M 18s
99400K .......... .......... .......... .......... .......... 37% 16.3M 18s
99450K .......... .......... .......... .......... .......... 37% 10.2M 18s
99500K .......... .......... .......... .......... .......... 37% 11.2M 18s
99550K .......... .......... .......... .......... .......... 37% 12.1M 18s
99600K .......... .......... .......... .......... .......... 37% 10.2M 18s
99650K .......... .......... .......... .......... .......... 37% 12.0M 18s
99700K .......... .......... .......... .......... .......... 37% 11.3M 18s
99750K .......... .......... .......... .......... .......... 37% 16.5M 18s
99800K .......... .......... .......... .......... .......... 37% 35.6M 18s
99850K .......... .......... .......... .......... .......... 37% 17.3M 18s
99900K .......... .......... .......... .......... .......... 37% 129M 18s
99950K .......... .......... .......... .......... .......... 37% 77.0M 18s
100000K .......... .......... .......... .......... .......... 37% 20.8M 18s
100050K .......... .......... .......... .......... .......... 37% 65.3M 18s
100100K .......... .......... .......... .......... .......... 37% 35.2M 18s
100150K .......... .......... .......... .......... .......... 37% 31.0M 18s
100200K .......... .......... .......... .......... .......... 37% 26.2M 17s
100250K .......... .......... .......... .......... .......... 37% 24.9M 17s
100300K .......... .......... .......... .......... .......... 37% 26.5M 17s
100350K .......... .......... .......... .......... .......... 37% 30.6M 17s
100400K .......... .......... .......... .......... .......... 37% 27.7M 17s
100450K .......... .......... .......... .......... .......... 37% 28.4M 17s
100500K .......... .......... .......... .......... .......... 37% 19.9M 17s
100550K .......... .......... .......... .......... .......... 37% 46.1M 17s
100600K .......... .......... .......... .......... .......... 37% 21.3M 17s
100650K .......... .......... .......... .......... .......... 37% 34.2M 17s
100700K .......... .......... .......... .......... .......... 37% 20.1M 17s
100750K .......... .......... .......... .......... .......... 37% 20.7M 17s
100800K .......... .......... .......... .......... .......... 37% 14.9M 17s
100850K .......... .......... .......... .......... .......... 37% 8.79M 17s
100900K .......... .......... .......... .......... .......... 37% 18.4M 17s
100950K .......... .......... .......... .......... .......... 38% 5.37M 17s
101000K .......... .......... .......... .......... .......... 38% 256M 17s
101050K .......... .......... .......... .......... .......... 38% 20.9M 17s
101100K .......... .......... .......... .......... .......... 38% 9.82M 17s
101150K .......... .......... .......... .......... .......... 38% 14.4M 17s
101200K .......... .......... .......... .......... .......... 38% 10.6M 17s
101250K .......... .......... .......... .......... .......... 38% 15.1M 17s
101300K .......... .......... .......... .......... .......... 38% 13.8M 17s
101350K .......... .......... .......... .......... .......... 38% 12.2M 17s
101400K .......... .......... .......... .......... .......... 38% 89.3M 17s
101450K .......... .......... .......... .......... .......... 38% 16.7M 17s
101500K .......... .......... .......... .......... .......... 38% 57.4M 17s
101550K .......... .......... .......... .......... .......... 38% 10.4M 17s
101600K .......... .......... .......... .......... .......... 38% 24.6M 17s
101650K .......... .......... .......... .......... .......... 38% 19.5M 17s
101700K .......... .......... .......... .......... .......... 38% 9.04M 17s
101750K .......... .......... .......... .......... .......... 38% 10.6M 17s
101800K .......... .......... .......... .......... .......... 38% 14.7M 17s
101850K .......... .......... .......... .......... .......... 38% 12.7M 17s
101900K .......... .......... .......... .......... .......... 38% 12.9M 17s
101950K .......... .......... .......... .......... .......... 38% 8.07M 17s
102000K .......... .......... .......... .......... .......... 38% 9.01M 17s
102050K .......... .......... .......... .......... .......... 38% 7.82M 17s
102100K .......... .......... .......... .......... .......... 38% 9.90M 17s
102150K .......... .......... .......... .......... .......... 38% 12.9M 17s
102200K .......... .......... .......... .......... .......... 38% 8.55M 17s
102250K .......... .......... .......... .......... .......... 38% 11.5M 17s
102300K .......... .......... .......... .......... .......... 38% 6.90M 17s
102350K .......... .......... .......... .......... .......... 38% 8.11M 17s
102400K .......... .......... .......... .......... .......... 38% 10.4M 17s
102450K .......... .......... .......... .......... .......... 38% 9.71M 17s
102500K .......... .......... .......... .......... .......... 38% 9.27M 17s
102550K .......... .......... .......... .......... .......... 38% 13.6M 17s
102600K .......... .......... .......... .......... .......... 38% 13.4M 17s
102650K .......... .......... .......... .......... .......... 38% 13.3M 17s
102700K .......... .......... .......... .......... .......... 38% 8.26M 17s
102750K .......... .......... .......... .......... .......... 38% 9.65M 17s
102800K .......... .......... .......... .......... .......... 38% 7.27M 17s
102850K .......... .......... .......... .......... .......... 38% 5.76M 17s
102900K .......... .......... .......... .......... .......... 38% 7.91M 17s
102950K .......... .......... .......... .......... .......... 38% 6.48M 17s
103000K .......... .......... .......... .......... .......... 38% 9.15M 17s
103050K .......... .......... .......... .......... .......... 38% 18.2M 17s
103100K .......... .......... .......... .......... .......... 38% 17.6M 17s
103150K .......... .......... .......... .......... .......... 38% 22.9M 17s
103200K .......... .......... .......... .......... .......... 38% 28.1M 17s
103250K .......... .......... .......... .......... .......... 38% 15.7M 17s
103300K .......... .......... .......... .......... .......... 38% 18.1M 17s
103350K .......... .......... .......... .......... .......... 38% 11.6M 17s
103400K .......... .......... .......... .......... .......... 38% 20.3M 17s
103450K .......... .......... .......... .......... .......... 38% 12.3M 17s
103500K .......... .......... .......... .......... .......... 38% 15.2M 17s
103550K .......... .......... .......... .......... .......... 38% 13.0M 17s
103600K .......... .......... .......... .......... .......... 38% 13.6M 17s
103650K .......... .......... .......... .......... .......... 39% 13.4M 17s
103700K .......... .......... .......... .......... .......... 39% 9.88M 17s
103750K .......... .......... .......... .......... .......... 39% 10.1M 17s
103800K .......... .......... .......... .......... .......... 39% 8.22M 17s
103850K .......... .......... .......... .......... .......... 39% 6.35M 17s
103900K .......... .......... .......... .......... .......... 39% 12.6M 17s
103950K .......... .......... .......... .......... .......... 39% 9.05M 17s
104000K .......... .......... .......... .......... .......... 39% 17.6M 17s
104050K .......... .......... .......... .......... .......... 39% 10.3M 17s
104100K .......... .......... .......... .......... .......... 39% 8.40M 17s
104150K .......... .......... .......... .......... .......... 39% 9.45M 17s
104200K .......... .......... .......... .......... .......... 39% 6.57M 17s
104250K .......... .......... .......... .......... .......... 39% 12.3M 17s
104300K .......... .......... .......... .......... .......... 39% 252M 17s
104350K .......... .......... .......... .......... .......... 39% 8.45M 17s
104400K .......... .......... .......... .......... .......... 39% 244M 17s
104450K .......... .......... .......... .......... .......... 39% 12.3M 17s
104500K .......... .......... .......... .......... .......... 39% 31.3M 17s
104550K .......... .......... .......... .......... .......... 39% 4.63M 17s
104600K .......... .......... .......... .......... .......... 39% 58.0M 17s
104650K .......... .......... .......... .......... .......... 39% 12.5M 17s
104700K .......... .......... .......... .......... .......... 39% 25.5M 17s
104750K .......... .......... .......... .......... .......... 39% 11.8M 17s
104800K .......... .......... .......... .......... .......... 39% 12.1M 17s
104850K .......... .......... .......... .......... .......... 39% 8.17M 17s
104900K .......... .......... .......... .......... .......... 39% 67.6M 17s
104950K .......... .......... .......... .......... .......... 39% 7.70M 17s
105000K .......... .......... .......... .......... .......... 39% 14.4M 17s
105050K .......... .......... .......... .......... .......... 39% 32.4M 17s
105100K .......... .......... .......... .......... .......... 39% 12.8M 17s
105150K .......... .......... .......... .......... .......... 39% 21.2M 17s
105200K .......... .......... .......... .......... .......... 39% 12.4M 17s
105250K .......... .......... .......... .......... .......... 39% 6.01M 17s
105300K .......... .......... .......... .......... .......... 39% 118M 17s
105350K .......... .......... .......... .......... .......... 39% 9.33M 17s
105400K .......... .......... .......... .......... .......... 39% 9.26M 17s
105450K .......... .......... .......... .......... .......... 39% 6.25M 17s
105500K .......... .......... .......... .......... .......... 39% 7.79M 17s
105550K .......... .......... .......... .......... .......... 39% 7.43M 17s
105600K .......... .......... .......... .......... .......... 39% 7.95M 17s
105650K .......... .......... .......... .......... .......... 39% 17.5M 17s
105700K .......... .......... .......... .......... .......... 39% 15.5M 17s
105750K .......... .......... .......... .......... .......... 39% 16.7M 17s
105800K .......... .......... .......... .......... .......... 39% 13.0M 17s
105850K .......... .......... .......... .......... .......... 39% 14.7M 17s
105900K .......... .......... .......... .......... .......... 39% 16.5M 17s
105950K .......... .......... .......... .......... .......... 39% 12.4M 17s
106000K .......... .......... .......... .......... .......... 39% 13.1M 17s
106050K .......... .......... .......... .......... .......... 39% 7.77M 17s
106100K .......... .......... .......... .......... .......... 39% 8.17M 17s
106150K .......... .......... .......... .......... .......... 39% 8.33M 17s
106200K .......... .......... .......... .......... .......... 39% 5.20M 17s
106250K .......... .......... .......... .......... .......... 39% 4.17M 17s
106300K .......... .......... .......... .......... .......... 40% 4.78M 17s
106350K .......... .......... .......... .......... .......... 40% 6.35M 17s
106400K .......... .......... .......... .......... .......... 40% 6.86M 17s
106450K .......... .......... .......... .......... .......... 40% 4.69M 17s
106500K .......... .......... .......... .......... .......... 40% 5.06M 17s
106550K .......... .......... .......... .......... .......... 40% 3.83M 17s
106600K .......... .......... .......... .......... .......... 40% 4.39M 17s
106650K .......... .......... .......... .......... .......... 40% 5.89M 17s
106700K .......... .......... .......... .......... .......... 40% 5.69M 17s
106750K .......... .......... .......... .......... .......... 40% 22.9M 17s
106800K .......... .......... .......... .......... .......... 40% 21.8M 17s
106850K .......... .......... .......... .......... .......... 40% 16.8M 17s
106900K .......... .......... .......... .......... .......... 40% 17.2M 17s
106950K .......... .......... .......... .......... .......... 40% 17.9M 17s
107000K .......... .......... .......... .......... .......... 40% 19.5M 17s
107050K .......... .......... .......... .......... .......... 40% 16.8M 17s
107100K .......... .......... .......... .......... .......... 40% 11.1M 17s
107150K .......... .......... .......... .......... .......... 40% 17.5M 17s
107200K .......... .......... .......... .......... .......... 40% 13.4M 17s
107250K .......... .......... .......... .......... .......... 40% 19.7M 17s
107300K .......... .......... .......... .......... .......... 40% 20.0M 17s
107350K .......... .......... .......... .......... .......... 40% 14.5M 17s
107400K .......... .......... .......... .......... .......... 40% 15.8M 17s
107450K .......... .......... .......... .......... .......... 40% 13.2M 17s
107500K .......... .......... .......... .......... .......... 40% 18.6M 17s
107550K .......... .......... .......... .......... .......... 40% 19.0M 17s
107600K .......... .......... .......... .......... .......... 40% 16.8M 16s
107650K .......... .......... .......... .......... .......... 40% 16.9M 16s
107700K .......... .......... .......... .......... .......... 40% 9.05M 16s
107750K .......... .......... .......... .......... .......... 40% 6.12M 16s
107800K .......... .......... .......... .......... .......... 40% 7.93M 16s
107850K .......... .......... .......... .......... .......... 40% 6.31M 16s
107900K .......... .......... .......... .......... .......... 40% 6.87M 16s
107950K .......... .......... .......... .......... .......... 40% 5.44M 16s
108000K .......... .......... .......... .......... .......... 40% 6.39M 16s
108050K .......... .......... .......... .......... .......... 40% 5.24M 16s
108100K .......... .......... .......... .......... .......... 40% 5.69M 16s
108150K .......... .......... .......... .......... .......... 40% 5.53M 16s
108200K .......... .......... .......... .......... .......... 40% 5.58M 16s
108250K .......... .......... .......... .......... .......... 40% 6.96M 16s
108300K .......... .......... .......... .......... .......... 40% 6.47M 16s
108350K .......... .......... .......... .......... .......... 40% 7.90M 16s
108400K .......... .......... .......... .......... .......... 40% 7.36M 16s
108450K .......... .......... .......... .......... .......... 40% 6.82M 16s
108500K .......... .......... .......... .......... .......... 40% 3.86M 16s
108550K .......... .......... .......... .......... .......... 40% 4.35M 16s
108600K .......... .......... .......... .......... .......... 40% 3.83M 16s
108650K .......... .......... .......... .......... .......... 40% 5.58M 16s
108700K .......... .......... .......... .......... .......... 40% 7.26M 16s
108750K .......... .......... .......... .......... .......... 40% 9.22M 16s
108800K .......... .......... .......... .......... .......... 40% 12.3M 16s
108850K .......... .......... .......... .......... .......... 40% 8.11M 16s
108900K .......... .......... .......... .......... .......... 40% 7.69M 16s
108950K .......... .......... .......... .......... .......... 41% 7.72M 16s
109000K .......... .......... .......... .......... .......... 41% 8.43M 16s
109050K .......... .......... .......... .......... .......... 41% 6.56M 16s
109100K .......... .......... .......... .......... .......... 41% 8.07M 16s
109150K .......... .......... .......... .......... .......... 41% 5.87M 16s
109200K .......... .......... .......... .......... .......... 41% 5.65M 16s
109250K .......... .......... .......... .......... .......... 41% 6.02M 16s
109300K .......... .......... .......... .......... .......... 41% 7.72M 16s
109350K .......... .......... .......... .......... .......... 41% 5.49M 16s
109400K .......... .......... .......... .......... .......... 41% 12.3M 16s
109450K .......... .......... .......... .......... .......... 41% 12.1M 16s
109500K .......... .......... .......... .......... .......... 41% 12.6M 16s
109550K .......... .......... .......... .......... .......... 41% 13.4M 16s
109600K .......... .......... .......... .......... .......... 41% 11.1M 16s
109650K .......... .......... .......... .......... .......... 41% 13.2M 16s
109700K .......... .......... .......... .......... .......... 41% 12.1M 16s
109750K .......... .......... .......... .......... .......... 41% 9.95M 16s
109800K .......... .......... .......... .......... .......... 41% 12.3M 16s
109850K .......... .......... .......... .......... .......... 41% 9.35M 16s
109900K .......... .......... .......... .......... .......... 41% 5.69M 16s
109950K .......... .......... .......... .......... .......... 41% 5.08M 16s
110000K .......... .......... .......... .......... .......... 41% 6.86M 16s
110050K .......... .......... .......... .......... .......... 41% 5.77M 16s
110100K .......... .......... .......... .......... .......... 41% 5.37M 16s
110150K .......... .......... .......... .......... .......... 41% 5.56M 16s
110200K .......... .......... .......... .......... .......... 41% 5.59M 16s
110250K .......... .......... .......... .......... .......... 41% 7.12M 16s
110300K .......... .......... .......... .......... .......... 41% 6.92M 16s
110350K .......... .......... .......... .......... .......... 41% 7.60M 16s
110400K .......... .......... .......... .......... .......... 41% 14.4M 16s
110450K .......... .......... .......... .......... .......... 41% 10.4M 16s
110500K .......... .......... .......... .......... .......... 41% 16.2M 16s
110550K .......... .......... .......... .......... .......... 41% 11.2M 16s
110600K .......... .......... .......... .......... .......... 41% 7.22M 16s
110650K .......... .......... .......... .......... .......... 41% 6.12M 16s
110700K .......... .......... .......... .......... .......... 41% 6.52M 16s
110750K .......... .......... .......... .......... .......... 41% 8.75M 16s
110800K .......... .......... .......... .......... .......... 41% 10.2M 16s
110850K .......... .......... .......... .......... .......... 41% 6.68M 16s
110900K .......... .......... .......... .......... .......... 41% 12.8M 16s
110950K .......... .......... .......... .......... .......... 41% 13.8M 16s
111000K .......... .......... .......... .......... .......... 41% 14.8M 16s
111050K .......... .......... .......... .......... .......... 41% 12.8M 16s
111100K .......... .......... .......... .......... .......... 41% 8.91M 16s
111150K .......... .......... .......... .......... .......... 41% 25.7M 16s
111200K .......... .......... .......... .......... .......... 41% 10.8M 16s
111250K .......... .......... .......... .......... .......... 41% 11.7M 16s
111300K .......... .......... .......... .......... .......... 41% 10.7M 16s
111350K .......... .......... .......... .......... .......... 41% 9.74M 16s
111400K .......... .......... .......... .......... .......... 41% 9.99M 16s
111450K .......... .......... .......... .......... .......... 41% 5.54M 16s
111500K .......... .......... .......... .......... .......... 41% 1.36M 16s
111550K .......... .......... .......... .......... .......... 41% 3.48M 16s
111600K .......... .......... .......... .......... .......... 42% 2.91M 16s
111650K .......... .......... .......... .......... .......... 42% 3.54M 16s
111700K .......... .......... .......... .......... .......... 42% 3.19M 16s
111750K .......... .......... .......... .......... .......... 42% 16.4M 16s
111800K .......... .......... .......... .......... .......... 42% 13.6M 16s
111850K .......... .......... .......... .......... .......... 42% 16.9M 16s
111900K .......... .......... .......... .......... .......... 42% 51.1M 16s
111950K .......... .......... .......... .......... .......... 42% 49.5M 16s
112000K .......... .......... .......... .......... .......... 42% 54.2M 16s
112050K .......... .......... .......... .......... .......... 42% 25.9M 16s
112100K .......... .......... .......... .......... .......... 42% 19.7M 16s
112150K .......... .......... .......... .......... .......... 42% 10.6M 16s
112200K .......... .......... .......... .......... .......... 42% 17.0M 16s
112250K .......... .......... .......... .......... .......... 42% 7.93M 16s
112300K .......... .......... .......... .......... .......... 42% 8.97M 16s
112350K .......... .......... .......... .......... .......... 42% 1.05M 16s
112400K .......... .......... .......... .......... .......... 42% 6.49M 16s
112450K .......... .......... .......... .......... .......... 42% 7.94M 16s
112500K .......... .......... .......... .......... .......... 42% 8.80M 16s
112550K .......... .......... .......... .......... .......... 42% 7.14M 16s
112600K .......... .......... .......... .......... .......... 42% 5.09M 16s
112650K .......... .......... .......... .......... .......... 42% 4.86M 16s
112700K .......... .......... .......... .......... .......... 42% 6.58M 16s
112750K .......... .......... .......... .......... .......... 42% 6.86M 16s
112800K .......... .......... .......... .......... .......... 42% 7.38M 16s
112850K .......... .......... .......... .......... .......... 42% 6.95M 16s
112900K .......... .......... .......... .......... .......... 42% 8.16M 16s
112950K .......... .......... .......... .......... .......... 42% 10.7M 16s
113000K .......... .......... .......... .......... .......... 42% 23.6M 16s
113050K .......... .......... .......... .......... .......... 42% 32.9M 16s
113100K .......... .......... .......... .......... .......... 42% 17.0M 16s
113150K .......... .......... .......... .......... .......... 42% 18.5M 16s
113200K .......... .......... .......... .......... .......... 42% 43.3M 16s
113250K .......... .......... .......... .......... .......... 42% 19.4M 16s
113300K .......... .......... .......... .......... .......... 42% 22.6M 16s
113350K .......... .......... .......... .......... .......... 42% 12.2M 16s
113400K .......... .......... .......... .......... .......... 42% 21.6M 16s
113450K .......... .......... .......... .......... .......... 42% 12.4M 16s
113500K .......... .......... .......... .......... .......... 42% 16.6M 16s
113550K .......... .......... .......... .......... .......... 42% 14.1M 16s
113600K .......... .......... .......... .......... .......... 42% 13.1M 16s
113650K .......... .......... .......... .......... .......... 42% 11.2M 16s
113700K .......... .......... .......... .......... .......... 42% 7.73M 16s
113750K .......... .......... .......... .......... .......... 42% 10.8M 16s
113800K .......... .......... .......... .......... .......... 42% 9.67M 16s
113850K .......... .......... .......... .......... .......... 42% 5.12M 16s
113900K .......... .......... .......... .......... .......... 42% 8.98M 16s
113950K .......... .......... .......... .......... .......... 42% 6.27M 16s
114000K .......... .......... .......... .......... .......... 42% 10.2M 16s
114050K .......... .......... .......... .......... .......... 42% 10.5M 16s
114100K .......... .......... .......... .......... .......... 42% 4.86M 16s
114150K .......... .......... .......... .......... .......... 42% 6.58M 16s
114200K .......... .......... .......... .......... .......... 42% 5.36M 16s
114250K .......... .......... .......... .......... .......... 43% 8.02M 16s
114300K .......... .......... .......... .......... .......... 43% 6.96M 16s
114350K .......... .......... .......... .......... .......... 43% 7.81M 16s
114400K .......... .......... .......... .......... .......... 43% 22.4M 16s
114450K .......... .......... .......... .......... .......... 43% 20.9M 16s
114500K .......... .......... .......... .......... .......... 43% 16.9M 16s
114550K .......... .......... .......... .......... .......... 43% 22.2M 16s
114600K .......... .......... .......... .......... .......... 43% 16.3M 16s
114650K .......... .......... .......... .......... .......... 43% 12.9M 16s
114700K .......... .......... .......... .......... .......... 43% 12.2M 16s
114750K .......... .......... .......... .......... .......... 43% 17.2M 16s
114800K .......... .......... .......... .......... .......... 43% 16.7M 16s
114850K .......... .......... .......... .......... .......... 43% 14.0M 16s
114900K .......... .......... .......... .......... .......... 43% 8.33M 16s
114950K .......... .......... .......... .......... .......... 43% 6.04M 16s
115000K .......... .......... .......... .......... .......... 43% 7.02M 16s
115050K .......... .......... .......... .......... .......... 43% 9.76M 16s
115100K .......... .......... .......... .......... .......... 43% 6.95M 16s
115150K .......... .......... .......... .......... .......... 43% 13.5M 16s
115200K .......... .......... .......... .......... .......... 43% 8.19M 16s
115250K .......... .......... .......... .......... .......... 43% 8.35M 16s
115300K .......... .......... .......... .......... .......... 43% 14.1M 16s
115350K .......... .......... .......... .......... .......... 43% 12.4M 16s
115400K .......... .......... .......... .......... .......... 43% 12.1M 16s
115450K .......... .......... .......... .......... .......... 43% 12.6M 16s
115500K .......... .......... .......... .......... .......... 43% 11.8M 16s
115550K .......... .......... .......... .......... .......... 43% 11.6M 16s
115600K .......... .......... .......... .......... .......... 43% 9.51M 16s
115650K .......... .......... .......... .......... .......... 43% 11.0M 16s
115700K .......... .......... .......... .......... .......... 43% 12.1M 16s
115750K .......... .......... .......... .......... .......... 43% 12.5M 16s
115800K .......... .......... .......... .......... .......... 43% 10.9M 16s
115850K .......... .......... .......... .......... .......... 43% 7.87M 16s
115900K .......... .......... .......... .......... .......... 43% 6.74M 16s
115950K .......... .......... .......... .......... .......... 43% 9.60M 16s
116000K .......... .......... .......... .......... .......... 43% 10.6M 16s
116050K .......... .......... .......... .......... .......... 43% 12.4M 16s
116100K .......... .......... .......... .......... .......... 43% 11.2M 16s
116150K .......... .......... .......... .......... .......... 43% 10.1M 16s
116200K .......... .......... .......... .......... .......... 43% 10.6M 16s
116250K .......... .......... .......... .......... .......... 43% 10.1M 16s
116300K .......... .......... .......... .......... .......... 43% 13.8M 16s
116350K .......... .......... .......... .......... .......... 43% 17.4M 16s
116400K .......... .......... .......... .......... .......... 43% 78.8M 16s
116450K .......... .......... .......... .......... .......... 43% 19.6M 16s
116500K .......... .......... .......... .......... .......... 43% 15.7M 16s
116550K .......... .......... .......... .......... .......... 43% 25.0M 16s
116600K .......... .......... .......... .......... .......... 43% 21.9M 16s
116650K .......... .......... .......... .......... .......... 43% 15.1M 16s
116700K .......... .......... .......... .......... .......... 43% 10.7M 16s
116750K .......... .......... .......... .......... .......... 43% 13.0M 16s
116800K .......... .......... .......... .......... .......... 43% 11.3M 16s
116850K .......... .......... .......... .......... .......... 43% 5.66M 16s
116900K .......... .......... .......... .......... .......... 44% 7.59M 16s
116950K .......... .......... .......... .......... .......... 44% 6.18M 16s
117000K .......... .......... .......... .......... .......... 44% 4.94M 16s
117050K .......... .......... .......... .......... .......... 44% 6.77M 16s
117100K .......... .......... .......... .......... .......... 44% 5.41M 16s
117150K .......... .......... .......... .......... .......... 44% 8.09M 16s
117200K .......... .......... .......... .......... .......... 44% 6.42M 16s
117250K .......... .......... .......... .......... .......... 44% 7.82M 16s
117300K .......... .......... .......... .......... .......... 44% 11.5M 16s
117350K .......... .......... .......... .......... .......... 44% 9.47M 16s
117400K .......... .......... .......... .......... .......... 44% 11.6M 16s
117450K .......... .......... .......... .......... .......... 44% 10.9M 16s
117500K .......... .......... .......... .......... .......... 44% 9.66M 16s
117550K .......... .......... .......... .......... .......... 44% 6.77M 16s
117600K .......... .......... .......... .......... .......... 44% 9.77M 16s
117650K .......... .......... .......... .......... .......... 44% 10.9M 16s
117700K .......... .......... .......... .......... .......... 44% 7.30M 16s
117750K .......... .......... .......... .......... .......... 44% 9.81M 16s
117800K .......... .......... .......... .......... .......... 44% 10.4M 16s
117850K .......... .......... .......... .......... .......... 44% 7.82M 16s
117900K .......... .......... .......... .......... .......... 44% 8.33M 16s
117950K .......... .......... .......... .......... .......... 44% 7.65M 16s
118000K .......... .......... .......... .......... .......... 44% 8.81M 16s
118050K .......... .......... .......... .......... .......... 44% 10.4M 16s
118100K .......... .......... .......... .......... .......... 44% 10.2M 16s
118150K .......... .......... .......... .......... .......... 44% 15.1M 16s
118200K .......... .......... .......... .......... .......... 44% 6.43M 16s
118250K .......... .......... .......... .......... .......... 44% 5.29M 16s
118300K .......... .......... .......... .......... .......... 44% 4.73M 16s
118350K .......... .......... .......... .......... .......... 44% 3.80M 16s
118400K .......... .......... .......... .......... .......... 44% 6.21M 16s
118450K .......... .......... .......... .......... .......... 44% 8.53M 16s
118500K .......... .......... .......... .......... .......... 44% 31.5M 16s
118550K .......... .......... .......... .......... .......... 44% 34.5M 16s
118600K .......... .......... .......... .......... .......... 44% 13.4M 16s
118650K .......... .......... .......... .......... .......... 44% 13.0M 16s
118700K .......... .......... .......... .......... .......... 44% 13.5M 16s
118750K .......... .......... .......... .......... .......... 44% 10.6M 16s
118800K .......... .......... .......... .......... .......... 44% 11.5M 16s
118850K .......... .......... .......... .......... .......... 44% 10.6M 16s
118900K .......... .......... .......... .......... .......... 44% 10.2M 16s
118950K .......... .......... .......... .......... .......... 44% 8.07M 16s
119000K .......... .......... .......... .......... .......... 44% 9.88M 16s
119050K .......... .......... .......... .......... .......... 44% 7.98M 16s
119100K .......... .......... .......... .......... .......... 44% 10.5M 15s
119150K .......... .......... .......... .......... .......... 44% 8.85M 15s
119200K .......... .......... .......... .......... .......... 44% 10.4M 15s
119250K .......... .......... .......... .......... .......... 44% 13.7M 15s
119300K .......... .......... .......... .......... .......... 44% 10.5M 15s
119350K .......... .......... .......... .......... .......... 44% 7.73M 15s
119400K .......... .......... .......... .......... .......... 44% 8.72M 15s
119450K .......... .......... .......... .......... .......... 44% 9.35M 15s
119500K .......... .......... .......... .......... .......... 44% 12.4M 15s
119550K .......... .......... .......... .......... .......... 44% 10.8M 15s
119600K .......... .......... .......... .......... .......... 45% 5.58M 15s
119650K .......... .......... .......... .......... .......... 45% 6.75M 15s
119700K .......... .......... .......... .......... .......... 45% 6.53M 15s
119750K .......... .......... .......... .......... .......... 45% 6.70M 15s
119800K .......... .......... .......... .......... .......... 45% 4.84M 15s
119850K .......... .......... .......... .......... .......... 45% 4.22M 15s
119900K .......... .......... .......... .......... .......... 45% 10.5M 15s
119950K .......... .......... .......... .......... .......... 45% 10.4M 15s
120000K .......... .......... .......... .......... .......... 45% 14.3M 15s
120050K .......... .......... .......... .......... .......... 45% 12.9M 15s
120100K .......... .......... .......... .......... .......... 45% 13.0M 15s
120150K .......... .......... .......... .......... .......... 45% 16.1M 15s
120200K .......... .......... .......... .......... .......... 45% 12.3M 15s
120250K .......... .......... .......... .......... .......... 45% 16.4M 15s
120300K .......... .......... .......... .......... .......... 45% 12.8M 15s
120350K .......... .......... .......... .......... .......... 45% 12.1M 15s
120400K .......... .......... .......... .......... .......... 45% 14.9M 15s
120450K .......... .......... .......... .......... .......... 45% 9.39M 15s
120500K .......... .......... .......... .......... .......... 45% 11.8M 15s
120550K .......... .......... .......... .......... .......... 45% 9.88M 15s
120600K .......... .......... .......... .......... .......... 45% 8.39M 15s
120650K .......... .......... .......... .......... .......... 45% 17.1M 15s
120700K .......... .......... .......... .......... .......... 45% 16.5M 15s
120750K .......... .......... .......... .......... .......... 45% 12.5M 15s
120800K .......... .......... .......... .......... .......... 45% 9.79M 15s
120850K .......... .......... .......... .......... .......... 45% 7.04M 15s
120900K .......... .......... .......... .......... .......... 45% 6.39M 15s
120950K .......... .......... .......... .......... .......... 45% 8.82M 15s
121000K .......... .......... .......... .......... .......... 45% 9.65M 15s
121050K .......... .......... .......... .......... .......... 45% 18.7M 15s
121100K .......... .......... .......... .......... .......... 45% 14.3M 15s
121150K .......... .......... .......... .......... .......... 45% 19.0M 15s
121200K .......... .......... .......... .......... .......... 45% 12.0M 15s
121250K .......... .......... .......... .......... .......... 45% 15.6M 15s
121300K .......... .......... .......... .......... .......... 45% 16.8M 15s
121350K .......... .......... .......... .......... .......... 45% 9.94M 15s
121400K .......... .......... .......... .......... .......... 45% 8.73M 15s
121450K .......... .......... .......... .......... .......... 45% 10.5M 15s
121500K .......... .......... .......... .......... .......... 45% 10.8M 15s
121550K .......... .......... .......... .......... .......... 45% 10.7M 15s
121600K .......... .......... .......... .......... .......... 45% 9.28M 15s
121650K .......... .......... .......... .......... .......... 45% 8.73M 15s
121700K .......... .......... .......... .......... .......... 45% 6.38M 15s
121750K .......... .......... .......... .......... .......... 45% 9.58M 15s
121800K .......... .......... .......... .......... .......... 45% 7.72M 15s
121850K .......... .......... .......... .......... .......... 45% 7.05M 15s
121900K .......... .......... .......... .......... .......... 45% 9.08M 15s
121950K .......... .......... .......... .......... .......... 45% 7.45M 15s
122000K .......... .......... .......... .......... .......... 45% 9.60M 15s
122050K .......... .......... .......... .......... .......... 45% 9.08M 15s
122100K .......... .......... .......... .......... .......... 45% 6.83M 15s
122150K .......... .......... .......... .......... .......... 45% 6.87M 15s
122200K .......... .......... .......... .......... .......... 45% 8.00M 15s
122250K .......... .......... .......... .......... .......... 46% 20.0M 15s
122300K .......... .......... .......... .......... .......... 46% 48.4M 15s
122350K .......... .......... .......... .......... .......... 46% 16.5M 15s
122400K .......... .......... .......... .......... .......... 46% 59.4M 15s
122450K .......... .......... .......... .......... .......... 46% 24.7M 15s
122500K .......... .......... .......... .......... .......... 46% 19.5M 15s
122550K .......... .......... .......... .......... .......... 46% 32.6M 15s
122600K .......... .......... .......... .......... .......... 46% 17.9M 15s
122650K .......... .......... .......... .......... .......... 46% 19.8M 15s
122700K .......... .......... .......... .......... .......... 46% 16.5M 15s
122750K .......... .......... .......... .......... .......... 46% 22.5M 15s
122800K .......... .......... .......... .......... .......... 46% 18.5M 15s
122850K .......... .......... .......... .......... .......... 46% 18.6M 15s
122900K .......... .......... .......... .......... .......... 46% 22.3M 15s
122950K .......... .......... .......... .......... .......... 46% 15.5M 15s
123000K .......... .......... .......... .......... .......... 46% 18.0M 15s
123050K .......... .......... .......... .......... .......... 46% 16.9M 15s
123100K .......... .......... .......... .......... .......... 46% 14.3M 15s
123150K .......... .......... .......... .......... .......... 46% 12.7M 15s
123200K .......... .......... .......... .......... .......... 46% 8.31M 15s
123250K .......... .......... .......... .......... .......... 46% 11.6M 15s
123300K .......... .......... .......... .......... .......... 46% 7.68M 15s
123350K .......... .......... .......... .......... .......... 46% 6.78M 15s
123400K .......... .......... .......... .......... .......... 46% 9.55M 15s
123450K .......... .......... .......... .......... .......... 46% 7.48M 15s
123500K .......... .......... .......... .......... .......... 46% 8.14M 15s
123550K .......... .......... .......... .......... .......... 46% 8.17M 15s
123600K .......... .......... .......... .......... .......... 46% 6.66M 15s
123650K .......... .......... .......... .......... .......... 46% 24.2M 15s
123700K .......... .......... .......... .......... .......... 46% 18.0M 15s
123750K .......... .......... .......... .......... .......... 46% 24.4M 15s
123800K .......... .......... .......... .......... .......... 46% 29.4M 15s
123850K .......... .......... .......... .......... .......... 46% 25.9M 15s
123900K .......... .......... .......... .......... .......... 46% 17.3M 15s
123950K .......... .......... .......... .......... .......... 46% 26.4M 15s
124000K .......... .......... .......... .......... .......... 46% 19.7M 15s
124050K .......... .......... .......... .......... .......... 46% 11.5M 15s
124100K .......... .......... .......... .......... .......... 46% 16.0M 15s
124150K .......... .......... .......... .......... .......... 46% 10.4M 15s
124200K .......... .......... .......... .......... .......... 46% 11.4M 15s
124250K .......... .......... .......... .......... .......... 46% 9.91M 15s
124300K .......... .......... .......... .......... .......... 46% 12.1M 15s
124350K .......... .......... .......... .......... .......... 46% 6.84M 15s
124400K .......... .......... .......... .......... .......... 46% 7.01M 15s
124450K .......... .......... .......... .......... .......... 46% 6.16M 15s
124500K .......... .......... .......... .......... .......... 46% 7.74M 15s
124550K .......... .......... .......... .......... .......... 46% 7.52M 15s
124600K .......... .......... .......... .......... .......... 46% 5.75M 15s
124650K .......... .......... .......... .......... .......... 46% 6.85M 15s
124700K .......... .......... .......... .......... .......... 46% 11.5M 15s
124750K .......... .......... .......... .......... .......... 46% 20.0M 15s
124800K .......... .......... .......... .......... .......... 46% 15.9M 15s
124850K .......... .......... .......... .......... .......... 46% 13.3M 15s
124900K .......... .......... .......... .......... .......... 47% 12.1M 15s
124950K .......... .......... .......... .......... .......... 47% 7.76M 15s
125000K .......... .......... .......... .......... .......... 47% 11.9M 15s
125050K .......... .......... .......... .......... .......... 47% 8.26M 15s
125100K .......... .......... .......... .......... .......... 47% 10.3M 15s
125150K .......... .......... .......... .......... .......... 47% 7.06M 15s
125200K .......... .......... .......... .......... .......... 47% 10.0M 15s
125250K .......... .......... .......... .......... .......... 47% 10.1M 15s
125300K .......... .......... .......... .......... .......... 47% 13.8M 15s
125350K .......... .......... .......... .......... .......... 47% 13.9M 15s
125400K .......... .......... .......... .......... .......... 47% 120M 15s
125450K .......... .......... .......... .......... .......... 47% 24.0M 15s
125500K .......... .......... .......... .......... .......... 47% 11.0M 15s
125550K .......... .......... .......... .......... .......... 47% 12.6M 15s
125600K .......... .......... .......... .......... .......... 47% 17.8M 15s
125650K .......... .......... .......... .......... .......... 47% 14.4M 15s
125700K .......... .......... .......... .......... .......... 47% 8.80M 15s
125750K .......... .......... .......... .......... .......... 47% 15.9M 15s
125800K .......... .......... .......... .......... .......... 47% 13.4M 15s
125850K .......... .......... .......... .......... .......... 47% 15.1M 15s
125900K .......... .......... .......... .......... .......... 47% 9.94M 15s
125950K .......... .......... .......... .......... .......... 47% 15.3M 15s
126000K .......... .......... .......... .......... .......... 47% 11.4M 15s
126050K .......... .......... .......... .......... .......... 47% 11.6M 15s
126100K .......... .......... .......... .......... .......... 47% 6.00M 15s
126150K .......... .......... .......... .......... .......... 47% 29.9M 15s
126200K .......... .......... .......... .......... .......... 47% 9.75M 15s
126250K .......... .......... .......... .......... .......... 47% 24.7M 15s
126300K .......... .......... .......... .......... .......... 47% 17.7M 15s
126350K .......... .......... .......... .......... .......... 47% 11.8M 15s
126400K .......... .......... .......... .......... .......... 47% 13.5M 15s
126450K .......... .......... .......... .......... .......... 47% 9.25M 15s
126500K .......... .......... .......... .......... .......... 47% 11.2M 15s
126550K .......... .......... .......... .......... .......... 47% 13.4M 15s
126600K .......... .......... .......... .......... .......... 47% 16.9M 15s
126650K .......... .......... .......... .......... .......... 47% 18.6M 15s
126700K .......... .......... .......... .......... .......... 47% 17.5M 15s
126750K .......... .......... .......... .......... .......... 47% 19.0M 15s
126800K .......... .......... .......... .......... .......... 47% 13.4M 15s
126850K .......... .......... .......... .......... .......... 47% 10.2M 15s
126900K .......... .......... .......... .......... .......... 47% 10.3M 15s
126950K .......... .......... .......... .......... .......... 47% 7.45M 15s
127000K .......... .......... .......... .......... .......... 47% 10.2M 15s
127050K .......... .......... .......... .......... .......... 47% 10.4M 15s
127100K .......... .......... .......... .......... .......... 47% 8.60M 15s
127150K .......... .......... .......... .......... .......... 47% 14.3M 15s
127200K .......... .......... .......... .......... .......... 47% 11.8M 14s
127250K .......... .......... .......... .......... .......... 47% 13.2M 14s
127300K .......... .......... .......... .......... .......... 47% 14.2M 14s
127350K .......... .......... .......... .......... .......... 47% 6.09M 14s
127400K .......... .......... .......... .......... .......... 47% 7.97M 14s
127450K .......... .......... .......... .......... .......... 47% 5.90M 14s
127500K .......... .......... .......... .......... .......... 47% 4.88M 14s
127550K .......... .......... .......... .......... .......... 48% 6.42M 14s
127600K .......... .......... .......... .......... .......... 48% 5.15M 14s
127650K .......... .......... .......... .......... .......... 48% 7.66M 14s
127700K .......... .......... .......... .......... .......... 48% 9.87M 14s
127750K .......... .......... .......... .......... .......... 48% 11.6M 14s
127800K .......... .......... .......... .......... .......... 48% 11.2M 14s
127850K .......... .......... .......... .......... .......... 48% 8.66M 14s
127900K .......... .......... .......... .......... .......... 48% 16.0M 14s
127950K .......... .......... .......... .......... .......... 48% 15.7M 14s
128000K .......... .......... .......... .......... .......... 48% 22.3M 14s
128050K .......... .......... .......... .......... .......... 48% 14.7M 14s
128100K .......... .......... .......... .......... .......... 48% 10.4M 14s
128150K .......... .......... .......... .......... .......... 48% 21.1M 14s
128200K .......... .......... .......... .......... .......... 48% 15.6M 14s
128250K .......... .......... .......... .......... .......... 48% 15.0M 14s
128300K .......... .......... .......... .......... .......... 48% 13.5M 14s
128350K .......... .......... .......... .......... .......... 48% 4.90M 14s
128400K .......... .......... .......... .......... .......... 48% 8.73M 14s
128450K .......... .......... .......... .......... .......... 48% 7.05M 14s
128500K .......... .......... .......... .......... .......... 48% 7.66M 14s
128550K .......... .......... .......... .......... .......... 48% 9.02M 14s
128600K .......... .......... .......... .......... .......... 48% 5.91M 14s
128650K .......... .......... .......... .......... .......... 48% 12.4M 14s
128700K .......... .......... .......... .......... .......... 48% 12.4M 14s
128750K .......... .......... .......... .......... .......... 48% 10.7M 14s
128800K .......... .......... .......... .......... .......... 48% 9.56M 14s
128850K .......... .......... .......... .......... .......... 48% 7.28M 14s
128900K .......... .......... .......... .......... .......... 48% 8.58M 14s
128950K .......... .......... .......... .......... .......... 48% 3.37M 14s
129000K .......... .......... .......... .......... .......... 48% 3.35M 14s
129050K .......... .......... .......... .......... .......... 48% 4.80M 14s
129100K .......... .......... .......... .......... .......... 48% 13.1M 14s
129150K .......... .......... .......... .......... .......... 48% 23.6M 14s
129200K .......... .......... .......... .......... .......... 48% 13.5M 14s
129250K .......... .......... .......... .......... .......... 48% 14.9M 14s
129300K .......... .......... .......... .......... .......... 48% 33.0M 14s
129350K .......... .......... .......... .......... .......... 48% 11.5M 14s
129400K .......... .......... .......... .......... .......... 48% 14.2M 14s
129450K .......... .......... .......... .......... .......... 48% 10.5M 14s
129500K .......... .......... .......... .......... .......... 48% 10.3M 14s
129550K .......... .......... .......... .......... .......... 48% 11.4M 14s
129600K .......... .......... .......... .......... .......... 48% 11.0M 14s
129650K .......... .......... .......... .......... .......... 48% 7.33M 14s
129700K .......... .......... .......... .......... .......... 48% 7.29M 14s
129750K .......... .......... .......... .......... .......... 48% 9.07M 14s
129800K .......... .......... .......... .......... .......... 48% 8.10M 14s
129850K .......... .......... .......... .......... .......... 48% 7.13M 14s
129900K .......... .......... .......... .......... .......... 48% 9.27M 14s
129950K .......... .......... .......... .......... .......... 48% 16.4M 14s
130000K .......... .......... .......... .......... .......... 48% 20.7M 14s
130050K .......... .......... .......... .......... .......... 48% 83.9M 14s
130100K .......... .......... .......... .......... .......... 48% 35.9M 14s
130150K .......... .......... .......... .......... .......... 48% 22.9M 14s
130200K .......... .......... .......... .......... .......... 49% 17.5M 14s
130250K .......... .......... .......... .......... .......... 49% 26.6M 14s
130300K .......... .......... .......... .......... .......... 49% 13.3M 14s
130350K .......... .......... .......... .......... .......... 49% 13.0M 14s
130400K .......... .......... .......... .......... .......... 49% 14.9M 14s
130450K .......... .......... .......... .......... .......... 49% 20.1M 14s
130500K .......... .......... .......... .......... .......... 49% 17.7M 14s
130550K .......... .......... .......... .......... .......... 49% 12.8M 14s
130600K .......... .......... .......... .......... .......... 49% 8.36M 14s
130650K .......... .......... .......... .......... .......... 49% 9.70M 14s
130700K .......... .......... .......... .......... .......... 49% 7.90M 14s
130750K .......... .......... .......... .......... .......... 49% 8.72M 14s
130800K .......... .......... .......... .......... .......... 49% 13.0M 14s
130850K .......... .......... .......... .......... .......... 49% 12.1M 14s
130900K .......... .......... .......... .......... .......... 49% 11.4M 14s
130950K .......... .......... .......... .......... .......... 49% 10.1M 14s
131000K .......... .......... .......... .......... .......... 49% 9.94M 14s
131050K .......... .......... .......... .......... .......... 49% 10.2M 14s
131100K .......... .......... .......... .......... .......... 49% 7.24M 14s
131150K .......... .......... .......... .......... .......... 49% 7.21M 14s
131200K .......... .......... .......... .......... .......... 49% 7.64M 14s
131250K .......... .......... .......... .......... .......... 49% 7.54M 14s
131300K .......... .......... .......... .......... .......... 49% 7.39M 14s
131350K .......... .......... .......... .......... .......... 49% 9.36M 14s
131400K .......... .......... .......... .......... .......... 49% 13.6M 14s
131450K .......... .......... .......... .......... .......... 49% 6.76M 14s
131500K .......... .......... .......... .......... .......... 49% 9.22M 14s
131550K .......... .......... .......... .......... .......... 49% 10.4M 14s
131600K .......... .......... .......... .......... .......... 49% 11.9M 14s
131650K .......... .......... .......... .......... .......... 49% 8.10M 14s
131700K .......... .......... .......... .......... .......... 49% 4.55M 14s
131750K .......... .......... .......... .......... .......... 49% 7.47M 14s
131800K .......... .......... .......... .......... .......... 49% 8.88M 14s
131850K .......... .......... .......... .......... .......... 49% 8.10M 14s
131900K .......... .......... .......... .......... .......... 49% 7.55M 14s
131950K .......... .......... .......... .......... .......... 49% 6.64M 14s
132000K .......... .......... .......... .......... .......... 49% 8.31M 14s
132050K .......... .......... .......... .......... .......... 49% 7.60M 14s
132100K .......... .......... .......... .......... .......... 49% 8.20M 14s
132150K .......... .......... .......... .......... .......... 49% 8.38M 14s
132200K .......... .......... .......... .......... .......... 49% 7.94M 14s
132250K .......... .......... .......... .......... .......... 49% 1.83M 14s
132300K .......... .......... .......... .......... .......... 49% 4.38M 14s
132350K .......... .......... .......... .......... .......... 49% 3.64M 14s
132400K .......... .......... .......... .......... .......... 49% 7.05M 14s
132450K .......... .......... .......... .......... .......... 49% 13.9M 14s
132500K .......... .......... .......... .......... .......... 49% 15.9M 14s
132550K .......... .......... .......... .......... .......... 49% 15.7M 14s
132600K .......... .......... .......... .......... .......... 49% 16.2M 14s
132650K .......... .......... .......... .......... .......... 49% 23.3M 14s
132700K .......... .......... .......... .......... .......... 49% 13.3M 14s
132750K .......... .......... .......... .......... .......... 49% 18.7M 14s
132800K .......... .......... .......... .......... .......... 49% 16.7M 14s
132850K .......... .......... .......... .......... .......... 50% 12.5M 14s
132900K .......... .......... .......... .......... .......... 50% 18.2M 14s
132950K .......... .......... .......... .......... .......... 50% 12.3M 14s
133000K .......... .......... .......... .......... .......... 50% 16.9M 14s
133050K .......... .......... .......... .......... .......... 50% 18.0M 14s
133100K .......... .......... .......... .......... .......... 50% 13.4M 14s
133150K .......... .......... .......... .......... .......... 50% 9.03M 14s
133200K .......... .......... .......... .......... .......... 50% 8.52M 14s
133250K .......... .......... .......... .......... .......... 50% 9.21M 14s
133300K .......... .......... .......... .......... .......... 50% 18.5M 14s
133350K .......... .......... .......... .......... .......... 50% 23.3M 14s
133400K .......... .......... .......... .......... .......... 50% 23.6M 14s
133450K .......... .......... .......... .......... .......... 50% 17.0M 14s
133500K .......... .......... .......... .......... .......... 50% 16.0M 14s
133550K .......... .......... .......... .......... .......... 50% 14.2M 14s
133600K .......... .......... .......... .......... .......... 50% 13.3M 14s
133650K .......... .......... .......... .......... .......... 50% 10.6M 14s
133700K .......... .......... .......... .......... .......... 50% 13.7M 14s
133750K .......... .......... .......... .......... .......... 50% 15.7M 14s
133800K .......... .......... .......... .......... .......... 50% 16.9M 14s
133850K .......... .......... .......... .......... .......... 50% 9.64M 14s
133900K .......... .......... .......... .......... .......... 50% 9.42M 14s
133950K .......... .......... .......... .......... .......... 50% 7.67M 14s
134000K .......... .......... .......... .......... .......... 50% 8.24M 14s
134050K .......... .......... .......... .......... .......... 50% 6.91M 14s
134100K .......... .......... .......... .......... .......... 50% 4.67M 14s
134150K .......... .......... .......... .......... .......... 50% 8.88M 14s
134200K .......... .......... .......... .......... .......... 50% 6.70M 14s
134250K .......... .......... .......... .......... .......... 50% 7.58M 14s
134300K .......... .......... .......... .......... .......... 50% 7.73M 14s
134350K .......... .......... .......... .......... .......... 50% 11.9M 14s
134400K .......... .......... .......... .......... .......... 50% 10.5M 14s
134450K .......... .......... .......... .......... .......... 50% 8.19M 14s
134500K .......... .......... .......... .......... .......... 50% 12.7M 14s
134550K .......... .......... .......... .......... .......... 50% 10.2M 14s
134600K .......... .......... .......... .......... .......... 50% 7.09M 14s
134650K .......... .......... .......... .......... .......... 50% 7.77M 14s
134700K .......... .......... .......... .......... .......... 50% 6.45M 14s
134750K .......... .......... .......... .......... .......... 50% 7.31M 14s
134800K .......... .......... .......... .......... .......... 50% 8.23M 14s
134850K .......... .......... .......... .......... .......... 50% 9.03M 14s
134900K .......... .......... .......... .......... .......... 50% 22.1M 14s
134950K .......... .......... .......... .......... .......... 50% 27.4M 14s
135000K .......... .......... .......... .......... .......... 50% 22.7M 14s
135050K .......... .......... .......... .......... .......... 50% 36.4M 14s
135100K .......... .......... .......... .......... .......... 50% 16.0M 14s
135150K .......... .......... .......... .......... .......... 50% 24.5M 14s
135200K .......... .......... .......... .......... .......... 50% 22.9M 14s
135250K .......... .......... .......... .......... .......... 50% 25.8M 14s
135300K .......... .......... .......... .......... .......... 50% 26.7M 14s
135350K .......... .......... .......... .......... .......... 50% 18.6M 14s
135400K .......... .......... .......... .......... .......... 50% 24.4M 14s
135450K .......... .......... .......... .......... .......... 50% 15.3M 14s
135500K .......... .......... .......... .......... .......... 51% 23.6M 14s
135550K .......... .......... .......... .......... .......... 51% 26.0M 14s
135600K .......... .......... .......... .......... .......... 51% 16.2M 14s
135650K .......... .......... .......... .......... .......... 51% 17.3M 14s
135700K .......... .......... .......... .......... .......... 51% 14.4M 14s
135750K .......... .......... .......... .......... .......... 51% 17.2M 14s
135800K .......... .......... .......... .......... .......... 51% 14.7M 14s
135850K .......... .......... .......... .......... .......... 51% 15.2M 14s
135900K .......... .......... .......... .......... .......... 51% 25.0M 14s
135950K .......... .......... .......... .......... .......... 51% 14.6M 14s
136000K .......... .......... .......... .......... .......... 51% 13.9M 14s
136050K .......... .......... .......... .......... .......... 51% 22.8M 14s
136100K .......... .......... .......... .......... .......... 51% 9.57M 14s
136150K .......... .......... .......... .......... .......... 51% 13.9M 13s
136200K .......... .......... .......... .......... .......... 51% 7.84M 13s
136250K .......... .......... .......... .......... .......... 51% 7.05M 13s
136300K .......... .......... .......... .......... .......... 51% 16.5M 13s
136350K .......... .......... .......... .......... .......... 51% 9.67M 13s
136400K .......... .......... .......... .......... .......... 51% 13.8M 13s
136450K .......... .......... .......... .......... .......... 51% 9.19M 13s
136500K .......... .......... .......... .......... .......... 51% 10.1M 13s
136550K .......... .......... .......... .......... .......... 51% 14.8M 13s
136600K .......... .......... .......... .......... .......... 51% 12.5M 13s
136650K .......... .......... .......... .......... .......... 51% 18.4M 13s
136700K .......... .......... .......... .......... .......... 51% 18.6M 13s
136750K .......... .......... .......... .......... .......... 51% 14.5M 13s
136800K .......... .......... .......... .......... .......... 51% 16.4M 13s
136850K .......... .......... .......... .......... .......... 51% 6.18M 13s
136900K .......... .......... .......... .......... .......... 51% 9.77M 13s
136950K .......... .......... .......... .......... .......... 51% 8.34M 13s
137000K .......... .......... .......... .......... .......... 51% 8.46M 13s
137050K .......... .......... .......... .......... .......... 51% 8.03M 13s
137100K .......... .......... .......... .......... .......... 51% 8.00M 13s
137150K .......... .......... .......... .......... .......... 51% 18.4M 13s
137200K .......... .......... .......... .......... .......... 51% 27.6M 13s
137250K .......... .......... .......... .......... .......... 51% 34.4M 13s
137300K .......... .......... .......... .......... .......... 51% 41.4M 13s
137350K .......... .......... .......... .......... .......... 51% 37.6M 13s
137400K .......... .......... .......... .......... .......... 51% 41.2M 13s
137450K .......... .......... .......... .......... .......... 51% 35.1M 13s
137500K .......... .......... .......... .......... .......... 51% 50.8M 13s
137550K .......... .......... .......... .......... .......... 51% 26.0M 13s
137600K .......... .......... .......... .......... .......... 51% 21.0M 13s
137650K .......... .......... .......... .......... .......... 51% 41.2M 13s
137700K .......... .......... .......... .......... .......... 51% 21.0M 13s
137750K .......... .......... .......... .......... .......... 51% 21.6M 13s
137800K .......... .......... .......... .......... .......... 51% 16.3M 13s
137850K .......... .......... .......... .......... .......... 51% 24.4M 13s
137900K .......... .......... .......... .......... .......... 51% 20.9M 13s
137950K .......... .......... .......... .......... .......... 51% 19.7M 13s
138000K .......... .......... .......... .......... .......... 51% 16.4M 13s
138050K .......... .......... .......... .......... .......... 51% 15.0M 13s
138100K .......... .......... .......... .......... .......... 51% 12.7M 13s
138150K .......... .......... .......... .......... .......... 51% 13.7M 13s
138200K .......... .......... .......... .......... .......... 52% 9.95M 13s
138250K .......... .......... .......... .......... .......... 52% 7.31M 13s
138300K .......... .......... .......... .......... .......... 52% 16.8M 13s
138350K .......... .......... .......... .......... .......... 52% 12.6M 13s
138400K .......... .......... .......... .......... .......... 52% 15.6M 13s
138450K .......... .......... .......... .......... .......... 52% 8.73M 13s
138500K .......... .......... .......... .......... .......... 52% 22.8M 13s
138550K .......... .......... .......... .......... .......... 52% 15.6M 13s
138600K .......... .......... .......... .......... .......... 52% 10.6M 13s
138650K .......... .......... .......... .......... .......... 52% 13.7M 13s
138700K .......... .......... .......... .......... .......... 52% 7.48M 13s
138750K .......... .......... .......... .......... .......... 52% 8.43M 13s
138800K .......... .......... .......... .......... .......... 52% 8.03M 13s
138850K .......... .......... .......... .......... .......... 52% 6.48M 13s
138900K .......... .......... .......... .......... .......... 52% 8.40M 13s
138950K .......... .......... .......... .......... .......... 52% 5.40M 13s
139000K .......... .......... .......... .......... .......... 52% 6.73M 13s
139050K .......... .......... .......... .......... .......... 52% 6.03M 13s
139100K .......... .......... .......... .......... .......... 52% 5.49M 13s
139150K .......... .......... .......... .......... .......... 52% 7.41M 13s
139200K .......... .......... .......... .......... .......... 52% 8.55M 13s
139250K .......... .......... .......... .......... .......... 52% 10.3M 13s
139300K .......... .......... .......... .......... .......... 52% 10.5M 13s
139350K .......... .......... .......... .......... .......... 52% 6.44M 13s
139400K .......... .......... .......... .......... .......... 52% 9.03M 13s
139450K .......... .......... .......... .......... .......... 52% 8.10M 13s
139500K .......... .......... .......... .......... .......... 52% 9.27M 13s
139550K .......... .......... .......... .......... .......... 52% 9.97M 13s
139600K .......... .......... .......... .......... .......... 52% 11.9M 13s
139650K .......... .......... .......... .......... .......... 52% 13.3M 13s
139700K .......... .......... .......... .......... .......... 52% 12.3M 13s
139750K .......... .......... .......... .......... .......... 52% 7.10M 13s
139800K .......... .......... .......... .......... .......... 52% 18.7M 13s
139850K .......... .......... .......... .......... .......... 52% 10.4M 13s
139900K .......... .......... .......... .......... .......... 52% 9.95M 13s
139950K .......... .......... .......... .......... .......... 52% 10.4M 13s
140000K .......... .......... .......... .......... .......... 52% 8.83M 13s
140050K .......... .......... .......... .......... .......... 52% 13.6M 13s
140100K .......... .......... .......... .......... .......... 52% 10.4M 13s
140150K .......... .......... .......... .......... .......... 52% 11.8M 13s
140200K .......... .......... .......... .......... .......... 52% 9.47M 13s
140250K .......... .......... .......... .......... .......... 52% 11.1M 13s
140300K .......... .......... .......... .......... .......... 52% 7.36M 13s
140350K .......... .......... .......... .......... .......... 52% 11.5M 13s
140400K .......... .......... .......... .......... .......... 52% 15.1M 13s
140450K .......... .......... .......... .......... .......... 52% 12.8M 13s
140500K .......... .......... .......... .......... .......... 52% 19.8M 13s
140550K .......... .......... .......... .......... .......... 52% 12.9M 13s
140600K .......... .......... .......... .......... .......... 52% 11.0M 13s
140650K .......... .......... .......... .......... .......... 52% 15.6M 13s
140700K .......... .......... .......... .......... .......... 52% 12.3M 13s
140750K .......... .......... .......... .......... .......... 52% 17.2M 13s
140800K .......... .......... .......... .......... .......... 52% 9.05M 13s
140850K .......... .......... .......... .......... .......... 53% 12.1M 13s
140900K .......... .......... .......... .......... .......... 53% 12.0M 13s
140950K .......... .......... .......... .......... .......... 53% 11.7M 13s
141000K .......... .......... .......... .......... .......... 53% 14.6M 13s
141050K .......... .......... .......... .......... .......... 53% 14.2M 13s
141100K .......... .......... .......... .......... .......... 53% 10.3M 13s
141150K .......... .......... .......... .......... .......... 53% 9.61M 13s
141200K .......... .......... .......... .......... .......... 53% 10.4M 13s
141250K .......... .......... .......... .......... .......... 53% 7.26M 13s
141300K .......... .......... .......... .......... .......... 53% 10.7M 13s
141350K .......... .......... .......... .......... .......... 53% 14.1M 13s
141400K .......... .......... .......... .......... .......... 53% 11.2M 13s
141450K .......... .......... .......... .......... .......... 53% 12.9M 13s
141500K .......... .......... .......... .......... .......... 53% 9.95M 13s
141550K .......... .......... .......... .......... .......... 53% 11.5M 13s
141600K .......... .......... .......... .......... .......... 53% 11.1M 13s
141650K .......... .......... .......... .......... .......... 53% 10.9M 13s
141700K .......... .......... .......... .......... .......... 53% 9.63M 13s
141750K .......... .......... .......... .......... .......... 53% 13.0M 13s
141800K .......... .......... .......... .......... .......... 53% 13.0M 13s
141850K .......... .......... .......... .......... .......... 53% 12.0M 13s
141900K .......... .......... .......... .......... .......... 53% 13.4M 13s
141950K .......... .......... .......... .......... .......... 53% 18.2M 13s
142000K .......... .......... .......... .......... .......... 53% 24.6M 13s
142050K .......... .......... .......... .......... .......... 53% 59.0M 13s
142100K .......... .......... .......... .......... .......... 53% 18.2M 13s
142150K .......... .......... .......... .......... .......... 53% 208M 13s
142200K .......... .......... .......... .......... .......... 53% 19.8M 13s
142250K .......... .......... .......... .......... .......... 53% 63.4M 13s
142300K .......... .......... .......... .......... .......... 53% 25.4M 13s
142350K .......... .......... .......... .......... .......... 53% 18.6M 13s
142400K .......... .......... .......... .......... .......... 53% 23.6M 13s
142450K .......... .......... .......... .......... .......... 53% 21.2M 13s
142500K .......... .......... .......... .......... .......... 53% 20.9M 13s
142550K .......... .......... .......... .......... .......... 53% 19.3M 13s
142600K .......... .......... .......... .......... .......... 53% 21.2M 13s
142650K .......... .......... .......... .......... .......... 53% 25.9M 13s
142700K .......... .......... .......... .......... .......... 53% 22.7M 13s
142750K .......... .......... .......... .......... .......... 53% 22.1M 13s
142800K .......... .......... .......... .......... .......... 53% 27.6M 13s
142850K .......... .......... .......... .......... .......... 53% 26.9M 13s
142900K .......... .......... .......... .......... .......... 53% 25.5M 13s
142950K .......... .......... .......... .......... .......... 53% 20.2M 13s
143000K .......... .......... .......... .......... .......... 53% 35.6M 13s
143050K .......... .......... .......... .......... .......... 53% 25.8M 13s
143100K .......... .......... .......... .......... .......... 53% 18.8M 13s
143150K .......... .......... .......... .......... .......... 53% 19.7M 13s
143200K .......... .......... .......... .......... .......... 53% 20.3M 13s
143250K .......... .......... .......... .......... .......... 53% 26.5M 13s
143300K .......... .......... .......... .......... .......... 53% 20.6M 13s
143350K .......... .......... .......... .......... .......... 53% 16.9M 13s
143400K .......... .......... .......... .......... .......... 53% 17.6M 13s
143450K .......... .......... .......... .......... .......... 53% 17.8M 13s
143500K .......... .......... .......... .......... .......... 54% 16.9M 13s
143550K .......... .......... .......... .......... .......... 54% 13.5M 13s
143600K .......... .......... .......... .......... .......... 54% 9.64M 13s
143650K .......... .......... .......... .......... .......... 54% 14.1M 13s
143700K .......... .......... .......... .......... .......... 54% 10.6M 13s
143750K .......... .......... .......... .......... .......... 54% 14.3M 13s
143800K .......... .......... .......... .......... .......... 54% 10.7M 13s
143850K .......... .......... .......... .......... .......... 54% 11.3M 13s
143900K .......... .......... .......... .......... .......... 54% 11.4M 13s
143950K .......... .......... .......... .......... .......... 54% 9.95M 13s
144000K .......... .......... .......... .......... .......... 54% 7.92M 13s
144050K .......... .......... .......... .......... .......... 54% 9.42M 12s
144100K .......... .......... .......... .......... .......... 54% 7.03M 12s
144150K .......... .......... .......... .......... .......... 54% 9.76M 12s
144200K .......... .......... .......... .......... .......... 54% 8.24M 12s
144250K .......... .......... .......... .......... .......... 54% 8.33M 12s
144300K .......... .......... .......... .......... .......... 54% 6.70M 12s
144350K .......... .......... .......... .......... .......... 54% 6.16M 12s
144400K .......... .......... .......... .......... .......... 54% 7.23M 12s
144450K .......... .......... .......... .......... .......... 54% 5.99M 12s
144500K .......... .......... .......... .......... .......... 54% 14.9M 12s
144550K .......... .......... .......... .......... .......... 54% 22.2M 12s
144600K .......... .......... .......... .......... .......... 54% 31.0M 12s
144650K .......... .......... .......... .......... .......... 54% 24.8M 12s
144700K .......... .......... .......... .......... .......... 54% 35.0M 12s
144750K .......... .......... .......... .......... .......... 54% 32.0M 12s
144800K .......... .......... .......... .......... .......... 54% 25.5M 12s
144850K .......... .......... .......... .......... .......... 54% 31.6M 12s
144900K .......... .......... .......... .......... .......... 54% 23.8M 12s
144950K .......... .......... .......... .......... .......... 54% 28.2M 12s
145000K .......... .......... .......... .......... .......... 54% 21.6M 12s
145050K .......... .......... .......... .......... .......... 54% 26.7M 12s
145100K .......... .......... .......... .......... .......... 54% 31.5M 12s
145150K .......... .......... .......... .......... .......... 54% 12.6M 12s
145200K .......... .......... .......... .......... .......... 54% 32.6M 12s
145250K .......... .......... .......... .......... .......... 54% 18.0M 12s
145300K .......... .......... .......... .......... .......... 54% 15.4M 12s
145350K .......... .......... .......... .......... .......... 54% 11.0M 12s
145400K .......... .......... .......... .......... .......... 54% 13.0M 12s
145450K .......... .......... .......... .......... .......... 54% 9.76M 12s
145500K .......... .......... .......... .......... .......... 54% 14.6M 12s
145550K .......... .......... .......... .......... .......... 54% 9.24M 12s
145600K .......... .......... .......... .......... .......... 54% 9.22M 12s
145650K .......... .......... .......... .......... .......... 54% 13.4M 12s
145700K .......... .......... .......... .......... .......... 54% 14.2M 12s
145750K .......... .......... .......... .......... .......... 54% 25.2M 12s
145800K .......... .......... .......... .......... .......... 54% 22.1M 12s
145850K .......... .......... .......... .......... .......... 54% 27.8M 12s
145900K .......... .......... .......... .......... .......... 54% 13.0M 12s
145950K .......... .......... .......... .......... .......... 54% 188M 12s
146000K .......... .......... .......... .......... .......... 54% 32.0M 12s
146050K .......... .......... .......... .......... .......... 54% 21.1M 12s
146100K .......... .......... .......... .......... .......... 54% 26.3M 12s
146150K .......... .......... .......... .......... .......... 55% 12.6M 12s
146200K .......... .......... .......... .......... .......... 55% 47.4M 12s
146250K .......... .......... .......... .......... .......... 55% 29.4M 12s
146300K .......... .......... .......... .......... .......... 55% 21.0M 12s
146350K .......... .......... .......... .......... .......... 55% 18.4M 12s
146400K .......... .......... .......... .......... .......... 55% 21.1M 12s
146450K .......... .......... .......... .......... .......... 55% 18.2M 12s
146500K .......... .......... .......... .......... .......... 55% 18.3M 12s
146550K .......... .......... .......... .......... .......... 55% 17.9M 12s
146600K .......... .......... .......... .......... .......... 55% 14.4M 12s
146650K .......... .......... .......... .......... .......... 55% 23.3M 12s
146700K .......... .......... .......... .......... .......... 55% 12.2M 12s
146750K .......... .......... .......... .......... .......... 55% 22.8M 12s
146800K .......... .......... .......... .......... .......... 55% 17.2M 12s
146850K .......... .......... .......... .......... .......... 55% 15.0M 12s
146900K .......... .......... .......... .......... .......... 55% 18.0M 12s
146950K .......... .......... .......... .......... .......... 55% 13.1M 12s
147000K .......... .......... .......... .......... .......... 55% 27.9M 12s
147050K .......... .......... .......... .......... .......... 55% 17.7M 12s
147100K .......... .......... .......... .......... .......... 55% 13.7M 12s
147150K .......... .......... .......... .......... .......... 55% 13.4M 12s
147200K .......... .......... .......... .......... .......... 55% 7.61M 12s
147250K .......... .......... .......... .......... .......... 55% 14.0M 12s
147300K .......... .......... .......... .......... .......... 55% 15.9M 12s
147350K .......... .......... .......... .......... .......... 55% 8.50M 12s
147400K .......... .......... .......... .......... .......... 55% 9.96M 12s
147450K .......... .......... .......... .......... .......... 55% 8.98M 12s
147500K .......... .......... .......... .......... .......... 55% 8.37M 12s
147550K .......... .......... .......... .......... .......... 55% 8.73M 12s
147600K .......... .......... .......... .......... .......... 55% 7.91M 12s
147650K .......... .......... .......... .......... .......... 55% 10.2M 12s
147700K .......... .......... .......... .......... .......... 55% 7.93M 12s
147750K .......... .......... .......... .......... .......... 55% 10.5M 12s
147800K .......... .......... .......... .......... .......... 55% 10.2M 12s
147850K .......... .......... .......... .......... .......... 55% 9.67M 12s
147900K .......... .......... .......... .......... .......... 55% 11.0M 12s
147950K .......... .......... .......... .......... .......... 55% 11.6M 12s
148000K .......... .......... .......... .......... .......... 55% 11.5M 12s
148050K .......... .......... .......... .......... .......... 55% 11.8M 12s
148100K .......... .......... .......... .......... .......... 55% 19.9M 12s
148150K .......... .......... .......... .......... .......... 55% 18.4M 12s
148200K .......... .......... .......... .......... .......... 55% 71.4M 12s
148250K .......... .......... .......... .......... .......... 55% 20.7M 12s
148300K .......... .......... .......... .......... .......... 55% 74.1M 12s
148350K .......... .......... .......... .......... .......... 55% 24.8M 12s
148400K .......... .......... .......... .......... .......... 55% 30.7M 12s
148450K .......... .......... .......... .......... .......... 55% 28.9M 12s
148500K .......... .......... .......... .......... .......... 55% 19.3M 12s
148550K .......... .......... .......... .......... .......... 55% 63.9M 12s
148600K .......... .......... .......... .......... .......... 55% 19.9M 12s
148650K .......... .......... .......... .......... .......... 55% 30.1M 12s
148700K .......... .......... .......... .......... .......... 55% 23.4M 12s
148750K .......... .......... .......... .......... .......... 55% 20.2M 12s
148800K .......... .......... .......... .......... .......... 56% 18.4M 12s
148850K .......... .......... .......... .......... .......... 56% 23.9M 12s
148900K .......... .......... .......... .......... .......... 56% 12.7M 12s
148950K .......... .......... .......... .......... .......... 56% 30.0M 12s
149000K .......... .......... .......... .......... .......... 56% 14.2M 12s
149050K .......... .......... .......... .......... .......... 56% 13.2M 12s
149100K .......... .......... .......... .......... .......... 56% 13.0M 12s
149150K .......... .......... .......... .......... .......... 56% 13.1M 12s
149200K .......... .......... .......... .......... .......... 56% 12.9M 12s
149250K .......... .......... .......... .......... .......... 56% 16.2M 12s
149300K .......... .......... .......... .......... .......... 56% 10.9M 12s
149350K .......... .......... .......... .......... .......... 56% 15.4M 12s
149400K .......... .......... .......... .......... .......... 56% 15.6M 12s
149450K .......... .......... .......... .......... .......... 56% 13.4M 12s
149500K .......... .......... .......... .......... .......... 56% 9.97M 12s
149550K .......... .......... .......... .......... .......... 56% 11.9M 12s
149600K .......... .......... .......... .......... .......... 56% 10.9M 12s
149650K .......... .......... .......... .......... .......... 56% 11.9M 12s
149700K .......... .......... .......... .......... .......... 56% 4.37M 12s
149750K .......... .......... .......... .......... .......... 56% 17.1M 12s
149800K .......... .......... .......... .......... .......... 56% 7.01M 12s
149850K .......... .......... .......... .......... .......... 56% 6.55M 12s
149900K .......... .......... .......... .......... .......... 56% 11.8M 12s
149950K .......... .......... .......... .......... .......... 56% 22.1M 12s
150000K .......... .......... .......... .......... .......... 56% 20.5M 12s
150050K .......... .......... .......... .......... .......... 56% 57.5M 12s
150100K .......... .......... .......... .......... .......... 56% 19.4M 12s
150150K .......... .......... .......... .......... .......... 56% 18.6M 12s
150200K .......... .......... .......... .......... .......... 56% 47.9M 12s
150250K .......... .......... .......... .......... .......... 56% 24.0M 12s
150300K .......... .......... .......... .......... .......... 56% 20.3M 12s
150350K .......... .......... .......... .......... .......... 56% 24.5M 12s
150400K .......... .......... .......... .......... .......... 56% 20.2M 12s
150450K .......... .......... .......... .......... .......... 56% 20.4M 12s
150500K .......... .......... .......... .......... .......... 56% 22.2M 12s
150550K .......... .......... .......... .......... .......... 56% 13.9M 12s
150600K .......... .......... .......... .......... .......... 56% 14.9M 12s
150650K .......... .......... .......... .......... .......... 56% 16.2M 12s
150700K .......... .......... .......... .......... .......... 56% 9.79M 12s
150750K .......... .......... .......... .......... .......... 56% 9.83M 12s
150800K .......... .......... .......... .......... .......... 56% 8.14M 12s
150850K .......... .......... .......... .......... .......... 56% 10.6M 12s
150900K .......... .......... .......... .......... .......... 56% 11.1M 12s
150950K .......... .......... .......... .......... .......... 56% 8.18M 12s
151000K .......... .......... .......... .......... .......... 56% 10.3M 12s
151050K .......... .......... .......... .......... .......... 56% 8.52M 12s
151100K .......... .......... .......... .......... .......... 56% 9.88M 12s
151150K .......... .......... .......... .......... .......... 56% 9.00M 12s
151200K .......... .......... .......... .......... .......... 56% 7.65M 12s
151250K .......... .......... .......... .......... .......... 56% 16.8M 12s
151300K .......... .......... .......... .......... .......... 56% 18.5M 12s
151350K .......... .......... .......... .......... .......... 56% 13.6M 12s
151400K .......... .......... .......... .......... .......... 56% 14.6M 12s
151450K .......... .......... .......... .......... .......... 57% 17.2M 12s
151500K .......... .......... .......... .......... .......... 57% 15.1M 12s
151550K .......... .......... .......... .......... .......... 57% 15.9M 12s
151600K .......... .......... .......... .......... .......... 57% 4.42M 12s
151650K .......... .......... .......... .......... .......... 57% 9.08M 12s
151700K .......... .......... .......... .......... .......... 57% 8.06M 12s
151750K .......... .......... .......... .......... .......... 57% 10.8M 12s
151800K .......... .......... .......... .......... .......... 57% 6.59M 12s
151850K .......... .......... .......... .......... .......... 57% 5.29M 12s
151900K .......... .......... .......... .......... .......... 57% 9.00M 12s
151950K .......... .......... .......... .......... .......... 57% 8.40M 12s
152000K .......... .......... .......... .......... .......... 57% 14.3M 12s
152050K .......... .......... .......... .......... .......... 57% 15.8M 11s
152100K .......... .......... .......... .......... .......... 57% 9.63M 11s
152150K .......... .......... .......... .......... .......... 57% 12.6M 11s
152200K .......... .......... .......... .......... .......... 57% 9.28M 11s
152250K .......... .......... .......... .......... .......... 57% 9.22M 11s
152300K .......... .......... .......... .......... .......... 57% 8.66M 11s
152350K .......... .......... .......... .......... .......... 57% 7.87M 11s
152400K .......... .......... .......... .......... .......... 57% 7.09M 11s
152450K .......... .......... .......... .......... .......... 57% 6.66M 11s
152500K .......... .......... .......... .......... .......... 57% 8.19M 11s
152550K .......... .......... .......... .......... .......... 57% 7.53M 11s
152600K .......... .......... .......... .......... .......... 57% 7.54M 11s
152650K .......... .......... .......... .......... .......... 57% 12.4M 11s
152700K .......... .......... .......... .......... .......... 57% 9.78M 11s
152750K .......... .......... .......... .......... .......... 57% 10.3M 11s
152800K .......... .......... .......... .......... .......... 57% 10.2M 11s
152850K .......... .......... .......... .......... .......... 57% 6.59M 11s
152900K .......... .......... .......... .......... .......... 57% 8.74M 11s
152950K .......... .......... .......... .......... .......... 57% 6.58M 11s
153000K .......... .......... .......... .......... .......... 57% 8.31M 11s
153050K .......... .......... .......... .......... .......... 57% 5.84M 11s
153100K .......... .......... .......... .......... .......... 57% 6.58M 11s
153150K .......... .......... .......... .......... .......... 57% 6.95M 11s
153200K .......... .......... .......... .......... .......... 57% 10.6M 11s
153250K .......... .......... .......... .......... .......... 57% 13.3M 11s
153300K .......... .......... .......... .......... .......... 57% 9.30M 11s
153350K .......... .......... .......... .......... .......... 57% 13.1M 11s
153400K .......... .......... .......... .......... .......... 57% 11.7M 11s
153450K .......... .......... .......... .......... .......... 57% 9.42M 11s
153500K .......... .......... .......... .......... .......... 57% 14.5M 11s
153550K .......... .......... .......... .......... .......... 57% 14.8M 11s
153600K .......... .......... .......... .......... .......... 57% 16.7M 11s
153650K .......... .......... .......... .......... .......... 57% 18.0M 11s
153700K .......... .......... .......... .......... .......... 57% 19.2M 11s
153750K .......... .......... .......... .......... .......... 57% 18.0M 11s
153800K .......... .......... .......... .......... .......... 57% 25.3M 11s
153850K .......... .......... .......... .......... .......... 57% 14.9M 11s
153900K .......... .......... .......... .......... .......... 57% 32.0M 11s
153950K .......... .......... .......... .......... .......... 57% 17.2M 11s
154000K .......... .......... .......... .......... .......... 57% 23.0M 11s
154050K .......... .......... .......... .......... .......... 57% 16.6M 11s
154100K .......... .......... .......... .......... .......... 57% 18.8M 11s
154150K .......... .......... .......... .......... .......... 58% 13.8M 11s
154200K .......... .......... .......... .......... .......... 58% 15.3M 11s
154250K .......... .......... .......... .......... .......... 58% 11.2M 11s
154300K .......... .......... .......... .......... .......... 58% 14.3M 11s
154350K .......... .......... .......... .......... .......... 58% 12.1M 11s
154400K .......... .......... .......... .......... .......... 58% 14.3M 11s
154450K .......... .......... .......... .......... .......... 58% 10.5M 11s
154500K .......... .......... .......... .......... .......... 58% 13.5M 11s
154550K .......... .......... .......... .......... .......... 58% 14.2M 11s
154600K .......... .......... .......... .......... .......... 58% 10.6M 11s
154650K .......... .......... .......... .......... .......... 58% 10.9M 11s
154700K .......... .......... .......... .......... .......... 58% 10.7M 11s
154750K .......... .......... .......... .......... .......... 58% 9.08M 11s
154800K .......... .......... .......... .......... .......... 58% 9.29M 11s
154850K .......... .......... .......... .......... .......... 58% 6.66M 11s
154900K .......... .......... .......... .......... .......... 58% 9.37M 11s
154950K .......... .......... .......... .......... .......... 58% 7.83M 11s
155000K .......... .......... .......... .......... .......... 58% 10.8M 11s
155050K .......... .......... .......... .......... .......... 58% 11.2M 11s
155100K .......... .......... .......... .......... .......... 58% 9.17M 11s
155150K .......... .......... .......... .......... .......... 58% 8.80M 11s
155200K .......... .......... .......... .......... .......... 58% 5.74M 11s
155250K .......... .......... .......... .......... .......... 58% 5.48M 11s
155300K .......... .......... .......... .......... .......... 58% 3.85M 11s
155350K .......... .......... .......... .......... .......... 58% 4.18M 11s
155400K .......... .......... .......... .......... .......... 58% 5.24M 11s
155450K .......... .......... .......... .......... .......... 58% 6.98M 11s
155500K .......... .......... .......... .......... .......... 58% 12.5M 11s
155550K .......... .......... .......... .......... .......... 58% 18.4M 11s
155600K .......... .......... .......... .......... .......... 58% 15.8M 11s
155650K .......... .......... .......... .......... .......... 58% 18.5M 11s
155700K .......... .......... .......... .......... .......... 58% 13.4M 11s
155750K .......... .......... .......... .......... .......... 58% 16.3M 11s
155800K .......... .......... .......... .......... .......... 58% 16.5M 11s
155850K .......... .......... .......... .......... .......... 58% 16.7M 11s
155900K .......... .......... .......... .......... .......... 58% 11.2M 11s
155950K .......... .......... .......... .......... .......... 58% 6.94M 11s
156000K .......... .......... .......... .......... .......... 58% 7.91M 11s
156050K .......... .......... .......... .......... .......... 58% 7.53M 11s
156100K .......... .......... .......... .......... .......... 58% 6.42M 11s
156150K .......... .......... .......... .......... .......... 58% 11.3M 11s
156200K .......... .......... .......... .......... .......... 58% 6.39M 11s
156250K .......... .......... .......... .......... .......... 58% 7.33M 11s
156300K .......... .......... .......... .......... .......... 58% 6.98M 11s
156350K .......... .......... .......... .......... .......... 58% 6.09M 11s
156400K .......... .......... .......... .......... .......... 58% 4.61M 11s
156450K .......... .......... .......... .......... .......... 58% 2.97M 11s
156500K .......... .......... .......... .......... .......... 58% 3.46M 11s
156550K .......... .......... .......... .......... .......... 58% 12.0M 11s
156600K .......... .......... .......... .......... .......... 58% 13.2M 11s
156650K .......... .......... .......... .......... .......... 58% 14.7M 11s
156700K .......... .......... .......... .......... .......... 58% 7.55M 11s
156750K .......... .......... .......... .......... .......... 58% 15.1M 11s
156800K .......... .......... .......... .......... .......... 59% 7.10M 11s
156850K .......... .......... .......... .......... .......... 59% 6.16M 11s
156900K .......... .......... .......... .......... .......... 59% 9.43M 11s
156950K .......... .......... .......... .......... .......... 59% 10.5M 11s
157000K .......... .......... .......... .......... .......... 59% 10.3M 11s
157050K .......... .......... .......... .......... .......... 59% 9.28M 11s
157100K .......... .......... .......... .......... .......... 59% 6.86M 11s
157150K .......... .......... .......... .......... .......... 59% 6.03M 11s
157200K .......... .......... .......... .......... .......... 59% 4.35M 11s
157250K .......... .......... .......... .......... .......... 59% 2.97M 11s
157300K .......... .......... .......... .......... .......... 59% 2.46M 11s
157350K .......... .......... .......... .......... .......... 59% 10.4M 11s
157400K .......... .......... .......... .......... .......... 59% 33.0M 11s
157450K .......... .......... .......... .......... .......... 59% 18.6M 11s
157500K .......... .......... .......... .......... .......... 59% 16.8M 11s
157550K .......... .......... .......... .......... .......... 59% 13.1M 11s
157600K .......... .......... .......... .......... .......... 59% 8.11M 11s
157650K .......... .......... .......... .......... .......... 59% 10.5M 11s
157700K .......... .......... .......... .......... .......... 59% 9.79M 11s
157750K .......... .......... .......... .......... .......... 59% 11.7M 11s
157800K .......... .......... .......... .......... .......... 59% 11.1M 11s
157850K .......... .......... .......... .......... .......... 59% 12.8M 11s
157900K .......... .......... .......... .......... .......... 59% 16.1M 11s
157950K .......... .......... .......... .......... .......... 59% 20.1M 11s
158000K .......... .......... .......... .......... .......... 59% 19.9M 11s
158050K .......... .......... .......... .......... .......... 59% 16.1M 11s
158100K .......... .......... .......... .......... .......... 59% 9.72M 11s
158150K .......... .......... .......... .......... .......... 59% 9.44M 11s
158200K .......... .......... .......... .......... .......... 59% 10.1M 11s
158250K .......... .......... .......... .......... .......... 59% 13.9M 11s
158300K .......... .......... .......... .......... .......... 59% 9.81M 11s
158350K .......... .......... .......... .......... .......... 59% 7.54M 11s
158400K .......... .......... .......... .......... .......... 59% 9.49M 11s
158450K .......... .......... .......... .......... .......... 59% 5.48M 11s
158500K .......... .......... .......... .......... .......... 59% 14.6M 11s
158550K .......... .......... .......... .......... .......... 59% 8.05M 11s
158600K .......... .......... .......... .......... .......... 59% 8.22M 11s
158650K .......... .......... .......... .......... .......... 59% 11.4M 11s
158700K .......... .......... .......... .......... .......... 59% 6.50M 11s
158750K .......... .......... .......... .......... .......... 59% 8.96M 11s
158800K .......... .......... .......... .......... .......... 59% 10.5M 11s
158850K .......... .......... .......... .......... .......... 59% 9.53M 11s
158900K .......... .......... .......... .......... .......... 59% 14.6M 11s
158950K .......... .......... .......... .......... .......... 59% 11.8M 11s
159000K .......... .......... .......... .......... .......... 59% 6.74M 11s
159050K .......... .......... .......... .......... .......... 59% 20.4M 11s
159100K .......... .......... .......... .......... .......... 59% 8.64M 11s
159150K .......... .......... .......... .......... .......... 59% 15.2M 11s
159200K .......... .......... .......... .......... .......... 59% 11.3M 11s
159250K .......... .......... .......... .......... .......... 59% 11.1M 11s
159300K .......... .......... .......... .......... .......... 59% 9.80M 11s
159350K .......... .......... .......... .......... .......... 59% 9.18M 11s
159400K .......... .......... .......... .......... .......... 59% 10.8M 11s
159450K .......... .......... .......... .......... .......... 60% 7.96M 11s
159500K .......... .......... .......... .......... .......... 60% 13.9M 11s
159550K .......... .......... .......... .......... .......... 60% 16.6M 11s
159600K .......... .......... .......... .......... .......... 60% 18.5M 11s
159650K .......... .......... .......... .......... .......... 60% 16.2M 11s
159700K .......... .......... .......... .......... .......... 60% 16.7M 11s
159750K .......... .......... .......... .......... .......... 60% 13.0M 11s
159800K .......... .......... .......... .......... .......... 60% 6.82M 11s
159850K .......... .......... .......... .......... .......... 60% 7.79M 11s
159900K .......... .......... .......... .......... .......... 60% 10.6M 11s
159950K .......... .......... .......... .......... .......... 60% 5.70M 11s
160000K .......... .......... .......... .......... .......... 60% 6.66M 11s
160050K .......... .......... .......... .......... .......... 60% 6.61M 11s
160100K .......... .......... .......... .......... .......... 60% 3.77M 11s
160150K .......... .......... .......... .......... .......... 60% 8.43M 11s
160200K .......... .......... .......... .......... .......... 60% 12.3M 11s
160250K .......... .......... .......... .......... .......... 60% 87.7M 11s
160300K .......... .......... .......... .......... .......... 60% 29.0M 11s
160350K .......... .......... .......... .......... .......... 60% 23.1M 11s
160400K .......... .......... .......... .......... .......... 60% 34.4M 11s
160450K .......... .......... .......... .......... .......... 60% 15.4M 11s
160500K .......... .......... .......... .......... .......... 60% 13.4M 11s
160550K .......... .......... .......... .......... .......... 60% 9.92M 11s
160600K .......... .......... .......... .......... .......... 60% 8.28M 11s
160650K .......... .......... .......... .......... .......... 60% 7.58M 11s
160700K .......... .......... .......... .......... .......... 60% 6.31M 11s
160750K .......... .......... .......... .......... .......... 60% 8.42M 11s
160800K .......... .......... .......... .......... .......... 60% 8.13M 11s
160850K .......... .......... .......... .......... .......... 60% 13.8M 11s
160900K .......... .......... .......... .......... .......... 60% 27.7M 11s
160950K .......... .......... .......... .......... .......... 60% 32.0M 11s
161000K .......... .......... .......... .......... .......... 60% 13.0M 11s
161050K .......... .......... .......... .......... .......... 60% 68.0M 11s
161100K .......... .......... .......... .......... .......... 60% 16.2M 11s
161150K .......... .......... .......... .......... .......... 60% 25.5M 11s
161200K .......... .......... .......... .......... .......... 60% 12.1M 11s
161250K .......... .......... .......... .......... .......... 60% 16.5M 11s
161300K .......... .......... .......... .......... .......... 60% 14.1M 11s
161350K .......... .......... .......... .......... .......... 60% 12.6M 11s
161400K .......... .......... .......... .......... .......... 60% 16.4M 11s
161450K .......... .......... .......... .......... .......... 60% 12.4M 11s
161500K .......... .......... .......... .......... .......... 60% 8.13M 11s
161550K .......... .......... .......... .......... .......... 60% 9.97M 11s
161600K .......... .......... .......... .......... .......... 60% 9.66M 11s
161650K .......... .......... .......... .......... .......... 60% 16.9M 11s
161700K .......... .......... .......... .......... .......... 60% 10.5M 11s
161750K .......... .......... .......... .......... .......... 60% 15.5M 11s
161800K .......... .......... .......... .......... .......... 60% 13.3M 11s
161850K .......... .......... .......... .......... .......... 60% 9.86M 11s
161900K .......... .......... .......... .......... .......... 60% 11.1M 11s
161950K .......... .......... .......... .......... .......... 60% 11.6M 11s
162000K .......... .......... .......... .......... .......... 60% 16.6M 10s
162050K .......... .......... .......... .......... .......... 60% 26.4M 10s
162100K .......... .......... .......... .......... .......... 61% 41.3M 10s
162150K .......... .......... .......... .......... .......... 61% 80.7M 10s
162200K .......... .......... .......... .......... .......... 61% 14.9M 10s
162250K .......... .......... .......... .......... .......... 61% 177M 10s
162300K .......... .......... .......... .......... .......... 61% 33.2M 10s
162350K .......... .......... .......... .......... .......... 61% 163M 10s
162400K .......... .......... .......... .......... .......... 61% 37.5M 10s
162450K .......... .......... .......... .......... .......... 61% 27.5M 10s
162500K .......... .......... .......... .......... .......... 61% 31.2M 10s
162550K .......... .......... .......... .......... .......... 61% 51.6M 10s
162600K .......... .......... .......... .......... .......... 61% 24.4M 10s
162650K .......... .......... .......... .......... .......... 61% 52.7M 10s
162700K .......... .......... .......... .......... .......... 61% 27.1M 10s
162750K .......... .......... .......... .......... .......... 61% 60.6M 10s
162800K .......... .......... .......... .......... .......... 61% 29.8M 10s
162850K .......... .......... .......... .......... .......... 61% 27.3M 10s
162900K .......... .......... .......... .......... .......... 61% 42.7M 10s
162950K .......... .......... .......... .......... .......... 61% 29.4M 10s
163000K .......... .......... .......... .......... .......... 61% 43.3M 10s
163050K .......... .......... .......... .......... .......... 61% 27.9M 10s
163100K .......... .......... .......... .......... .......... 61% 17.7M 10s
163150K .......... .......... .......... .......... .......... 61% 74.1M 10s
163200K .......... .......... .......... .......... .......... 61% 14.8M 10s
163250K .......... .......... .......... .......... .......... 61% 18.6M 10s
163300K .......... .......... .......... .......... .......... 61% 10.1M 10s
163350K .......... .......... .......... .......... .......... 61% 13.7M 10s
163400K .......... .......... .......... .......... .......... 61% 8.63M 10s
163450K .......... .......... .......... .......... .......... 61% 9.19M 10s
163500K .......... .......... .......... .......... .......... 61% 9.57M 10s
163550K .......... .......... .......... .......... .......... 61% 13.3M 10s
163600K .......... .......... .......... .......... .......... 61% 10.2M 10s
163650K .......... .......... .......... .......... .......... 61% 10.3M 10s
163700K .......... .......... .......... .......... .......... 61% 136M 10s
163750K .......... .......... .......... .......... .......... 61% 30.4M 10s
163800K .......... .......... .......... .......... .......... 61% 13.2M 10s
163850K .......... .......... .......... .......... .......... 61% 9.09M 10s
163900K .......... .......... .......... .......... .......... 61% 11.3M 10s
163950K .......... .......... .......... .......... .......... 61% 8.62M 10s
164000K .......... .......... .......... .......... .......... 61% 11.3M 10s
164050K .......... .......... .......... .......... .......... 61% 9.03M 10s
164100K .......... .......... .......... .......... .......... 61% 10.2M 10s
164150K .......... .......... .......... .......... .......... 61% 17.0M 10s
164200K .......... .......... .......... .......... .......... 61% 11.3M 10s
164250K .......... .......... .......... .......... .......... 61% 15.2M 10s
164300K .......... .......... .......... .......... .......... 61% 25.5M 10s
164350K .......... .......... .......... .......... .......... 61% 14.6M 10s
164400K .......... .......... .......... .......... .......... 61% 15.6M 10s
164450K .......... .......... .......... .......... .......... 61% 13.8M 10s
164500K .......... .......... .......... .......... .......... 61% 13.4M 10s
164550K .......... .......... .......... .......... .......... 61% 9.99M 10s
164600K .......... .......... .......... .......... .......... 61% 7.01M 10s
164650K .......... .......... .......... .......... .......... 61% 8.51M 10s
164700K .......... .......... .......... .......... .......... 61% 8.19M 10s
164750K .......... .......... .......... .......... .......... 62% 8.29M 10s
164800K .......... .......... .......... .......... .......... 62% 6.13M 10s
164850K .......... .......... .......... .......... .......... 62% 8.59M 10s
164900K .......... .......... .......... .......... .......... 62% 25.3M 10s
164950K .......... .......... .......... .......... .......... 62% 19.3M 10s
165000K .......... .......... .......... .......... .......... 62% 31.8M 10s
165050K .......... .......... .......... .......... .......... 62% 43.1M 10s
165100K .......... .......... .......... .......... .......... 62% 34.1M 10s
165150K .......... .......... .......... .......... .......... 62% 26.8M 10s
165200K .......... .......... .......... .......... .......... 62% 23.1M 10s
165250K .......... .......... .......... .......... .......... 62% 28.6M 10s
165300K .......... .......... .......... .......... .......... 62% 18.9M 10s
165350K .......... .......... .......... .......... .......... 62% 17.2M 10s
165400K .......... .......... .......... .......... .......... 62% 16.1M 10s
165450K .......... .......... .......... .......... .......... 62% 12.0M 10s
165500K .......... .......... .......... .......... .......... 62% 14.4M 10s
165550K .......... .......... .......... .......... .......... 62% 12.8M 10s
165600K .......... .......... .......... .......... .......... 62% 5.11M 10s
165650K .......... .......... .......... .......... .......... 62% 18.0M 10s
165700K .......... .......... .......... .......... .......... 62% 8.27M 10s
165750K .......... .......... .......... .......... .......... 62% 13.0M 10s
165800K .......... .......... .......... .......... .......... 62% 10.6M 10s
165850K .......... .......... .......... .......... .......... 62% 7.41M 10s
165900K .......... .......... .......... .......... .......... 62% 11.1M 10s
165950K .......... .......... .......... .......... .......... 62% 10.9M 10s
166000K .......... .......... .......... .......... .......... 62% 12.2M 10s
166050K .......... .......... .......... .......... .......... 62% 12.1M 10s
166100K .......... .......... .......... .......... .......... 62% 9.30M 10s
166150K .......... .......... .......... .......... .......... 62% 21.6M 10s
166200K .......... .......... .......... .......... .......... 62% 16.5M 10s
166250K .......... .......... .......... .......... .......... 62% 21.2M 10s
166300K .......... .......... .......... .......... .......... 62% 17.7M 10s
166350K .......... .......... .......... .......... .......... 62% 12.4M 10s
166400K .......... .......... .......... .......... .......... 62% 10.8M 10s
166450K .......... .......... .......... .......... .......... 62% 9.75M 10s
166500K .......... .......... .......... .......... .......... 62% 11.3M 10s
166550K .......... .......... .......... .......... .......... 62% 8.89M 10s
166600K .......... .......... .......... .......... .......... 62% 8.00M 10s
166650K .......... .......... .......... .......... .......... 62% 8.56M 10s
166700K .......... .......... .......... .......... .......... 62% 7.89M 10s
166750K .......... .......... .......... .......... .......... 62% 9.75M 10s
166800K .......... .......... .......... .......... .......... 62% 9.93M 10s
166850K .......... .......... .......... .......... .......... 62% 8.26M 10s
166900K .......... .......... .......... .......... .......... 62% 9.75M 10s
166950K .......... .......... .......... .......... .......... 62% 6.41M 10s
167000K .......... .......... .......... .......... .......... 62% 7.27M 10s
167050K .......... .......... .......... .......... .......... 62% 6.77M 10s
167100K .......... .......... .......... .......... .......... 62% 7.61M 10s
167150K .......... .......... .......... .......... .......... 62% 5.88M 10s
167200K .......... .......... .......... .......... .......... 62% 7.52M 10s
167250K .......... .......... .......... .......... .......... 62% 8.79M 10s
167300K .......... .......... .......... .......... .......... 62% 6.53M 10s
167350K .......... .......... .......... .......... .......... 62% 5.31M 10s
167400K .......... .......... .......... .......... .......... 63% 6.53M 10s
167450K .......... .......... .......... .......... .......... 63% 15.1M 10s
167500K .......... .......... .......... .......... .......... 63% 26.4M 10s
167550K .......... .......... .......... .......... .......... 63% 29.0M 10s
167600K .......... .......... .......... .......... .......... 63% 38.9M 10s
167650K .......... .......... .......... .......... .......... 63% 24.2M 10s
167700K .......... .......... .......... .......... .......... 63% 28.7M 10s
167750K .......... .......... .......... .......... .......... 63% 20.4M 10s
167800K .......... .......... .......... .......... .......... 63% 25.6M 10s
167850K .......... .......... .......... .......... .......... 63% 24.7M 10s
167900K .......... .......... .......... .......... .......... 63% 15.9M 10s
167950K .......... .......... .......... .......... .......... 63% 35.4M 10s
168000K .......... .......... .......... .......... .......... 63% 18.1M 10s
168050K .......... .......... .......... .......... .......... 63% 16.9M 10s
168100K .......... .......... .......... .......... .......... 63% 22.5M 10s
168150K .......... .......... .......... .......... .......... 63% 21.2M 10s
168200K .......... .......... .......... .......... .......... 63% 21.6M 10s
168250K .......... .......... .......... .......... .......... 63% 31.8M 10s
168300K .......... .......... .......... .......... .......... 63% 18.3M 10s
168350K .......... .......... .......... .......... .......... 63% 16.7M 10s
168400K .......... .......... .......... .......... .......... 63% 17.8M 10s
168450K .......... .......... .......... .......... .......... 63% 10.4M 10s
168500K .......... .......... .......... .......... .......... 63% 9.15M 10s
168550K .......... .......... .......... .......... .......... 63% 14.5M 10s
168600K .......... .......... .......... .......... .......... 63% 7.82M 10s
168650K .......... .......... .......... .......... .......... 63% 7.30M 10s
168700K .......... .......... .......... .......... .......... 63% 8.03M 10s
168750K .......... .......... .......... .......... .......... 63% 9.39M 10s
168800K .......... .......... .......... .......... .......... 63% 7.38M 10s
168850K .......... .......... .......... .......... .......... 63% 8.93M 10s
168900K .......... .......... .......... .......... .......... 63% 8.52M 10s
168950K .......... .......... .......... .......... .......... 63% 9.97M 10s
169000K .......... .......... .......... .......... .......... 63% 14.0M 10s
169050K .......... .......... .......... .......... .......... 63% 16.0M 10s
169100K .......... .......... .......... .......... .......... 63% 16.2M 10s
169150K .......... .......... .......... .......... .......... 63% 11.8M 10s
169200K .......... .......... .......... .......... .......... 63% 12.3M 10s
169250K .......... .......... .......... .......... .......... 63% 13.8M 10s
169300K .......... .......... .......... .......... .......... 63% 11.1M 10s
169350K .......... .......... .......... .......... .......... 63% 21.1M 10s
169400K .......... .......... .......... .......... .......... 63% 19.6M 10s
169450K .......... .......... .......... .......... .......... 63% 14.2M 10s
169500K .......... .......... .......... .......... .......... 63% 16.4M 10s
169550K .......... .......... .......... .......... .......... 63% 18.9M 10s
169600K .......... .......... .......... .......... .......... 63% 13.2M 10s
169650K .......... .......... .......... .......... .......... 63% 14.3M 10s
169700K .......... .......... .......... .......... .......... 63% 11.4M 10s
169750K .......... .......... .......... .......... .......... 63% 17.0M 10s
169800K .......... .......... .......... .......... .......... 63% 14.7M 10s
169850K .......... .......... .......... .......... .......... 63% 10.2M 10s
169900K .......... .......... .......... .......... .......... 63% 13.9M 10s
169950K .......... .......... .......... .......... .......... 63% 6.30M 10s
170000K .......... .......... .......... .......... .......... 63% 7.64M 10s
170050K .......... .......... .......... .......... .......... 64% 6.63M 10s
170100K .......... .......... .......... .......... .......... 64% 6.03M 10s
170150K .......... .......... .......... .......... .......... 64% 5.72M 10s
170200K .......... .......... .......... .......... .......... 64% 3.19M 10s
170250K .......... .......... .......... .......... .......... 64% 3.56M 10s
170300K .......... .......... .......... .......... .......... 64% 4.48M 10s
170350K .......... .......... .......... .......... .......... 64% 5.76M 10s
170400K .......... .......... .......... .......... .......... 64% 11.9M 10s
170450K .......... .......... .......... .......... .......... 64% 9.34M 10s
170500K .......... .......... .......... .......... .......... 64% 9.75M 10s
170550K .......... .......... .......... .......... .......... 64% 8.64M 10s
170600K .......... .......... .......... .......... .......... 64% 7.65M 10s
170650K .......... .......... .......... .......... .......... 64% 9.70M 10s
170700K .......... .......... .......... .......... .......... 64% 7.75M 10s
170750K .......... .......... .......... .......... .......... 64% 7.99M 10s
170800K .......... .......... .......... .......... .......... 64% 9.20M 10s
170850K .......... .......... .......... .......... .......... 64% 4.78M 10s
170900K .......... .......... .......... .......... .......... 64% 10.6M 10s
170950K .......... .......... .......... .......... .......... 64% 10.5M 9s
171000K .......... .......... .......... .......... .......... 64% 8.86M 9s
171050K .......... .......... .......... .......... .......... 64% 11.7M 9s
171100K .......... .......... .......... .......... .......... 64% 9.53M 9s
171150K .......... .......... .......... .......... .......... 64% 12.2M 9s
171200K .......... .......... .......... .......... .......... 64% 13.5M 9s
171250K .......... .......... .......... .......... .......... 64% 16.3M 9s
171300K .......... .......... .......... .......... .......... 64% 13.0M 9s
171350K .......... .......... .......... .......... .......... 64% 15.2M 9s
171400K .......... .......... .......... .......... .......... 64% 15.1M 9s
171450K .......... .......... .......... .......... .......... 64% 17.6M 9s
171500K .......... .......... .......... .......... .......... 64% 15.1M 9s
171550K .......... .......... .......... .......... .......... 64% 12.9M 9s
171600K .......... .......... .......... .......... .......... 64% 6.94M 9s
171650K .......... .......... .......... .......... .......... 64% 9.02M 9s
171700K .......... .......... .......... .......... .......... 64% 6.95M 9s
171750K .......... .......... .......... .......... .......... 64% 5.43M 9s
171800K .......... .......... .......... .......... .......... 64% 15.2M 9s
171850K .......... .......... .......... .......... .......... 64% 13.3M 9s
171900K .......... .......... .......... .......... .......... 64% 13.5M 9s
171950K .......... .......... .......... .......... .......... 64% 11.4M 9s
172000K .......... .......... .......... .......... .......... 64% 12.4M 9s
172050K .......... .......... .......... .......... .......... 64% 15.6M 9s
172100K .......... .......... .......... .......... .......... 64% 9.33M 9s
172150K .......... .......... .......... .......... .......... 64% 12.0M 9s
172200K .......... .......... .......... .......... .......... 64% 15.7M 9s
172250K .......... .......... .......... .......... .......... 64% 12.8M 9s
172300K .......... .......... .......... .......... .......... 64% 12.1M 9s
172350K .......... .......... .......... .......... .......... 64% 17.4M 9s
172400K .......... .......... .......... .......... .......... 64% 10.9M 9s
172450K .......... .......... .......... .......... .......... 64% 12.5M 9s
172500K .......... .......... .......... .......... .......... 64% 14.3M 9s
172550K .......... .......... .......... .......... .......... 64% 9.88M 9s
172600K .......... .......... .......... .......... .......... 64% 12.1M 9s
172650K .......... .......... .......... .......... .......... 64% 13.7M 9s
172700K .......... .......... .......... .......... .......... 64% 9.49M 9s
172750K .......... .......... .......... .......... .......... 65% 8.88M 9s
172800K .......... .......... .......... .......... .......... 65% 7.21M 9s
172850K .......... .......... .......... .......... .......... 65% 7.55M 9s
172900K .......... .......... .......... .......... .......... 65% 8.84M 9s
172950K .......... .......... .......... .......... .......... 65% 8.72M 9s
173000K .......... .......... .......... .......... .......... 65% 15.6M 9s
173050K .......... .......... .......... .......... .......... 65% 12.7M 9s
173100K .......... .......... .......... .......... .......... 65% 10.4M 9s
173150K .......... .......... .......... .......... .......... 65% 8.49M 9s
173200K .......... .......... .......... .......... .......... 65% 8.55M 9s
173250K .......... .......... .......... .......... .......... 65% 9.09M 9s
173300K .......... .......... .......... .......... .......... 65% 9.74M 9s
173350K .......... .......... .......... .......... .......... 65% 10.0M 9s
173400K .......... .......... .......... .......... .......... 65% 11.9M 9s
173450K .......... .......... .......... .......... .......... 65% 11.2M 9s
173500K .......... .......... .......... .......... .......... 65% 12.3M 9s
173550K .......... .......... .......... .......... .......... 65% 13.0M 9s
173600K .......... .......... .......... .......... .......... 65% 10.7M 9s
173650K .......... .......... .......... .......... .......... 65% 9.71M 9s
173700K .......... .......... .......... .......... .......... 65% 11.5M 9s
173750K .......... .......... .......... .......... .......... 65% 13.5M 9s
173800K .......... .......... .......... .......... .......... 65% 16.4M 9s
173850K .......... .......... .......... .......... .......... 65% 15.6M 9s
173900K .......... .......... .......... .......... .......... 65% 11.4M 9s
173950K .......... .......... .......... .......... .......... 65% 14.1M 9s
174000K .......... .......... .......... .......... .......... 65% 18.9M 9s
174050K .......... .......... .......... .......... .......... 65% 18.5M 9s
174100K .......... .......... .......... .......... .......... 65% 16.2M 9s
174150K .......... .......... .......... .......... .......... 65% 22.2M 9s
174200K .......... .......... .......... .......... .......... 65% 20.4M 9s
174250K .......... .......... .......... .......... .......... 65% 22.8M 9s
174300K .......... .......... .......... .......... .......... 65% 22.3M 9s
174350K .......... .......... .......... .......... .......... 65% 10.5M 9s
174400K .......... .......... .......... .......... .......... 65% 19.0M 9s
174450K .......... .......... .......... .......... .......... 65% 17.4M 9s
174500K .......... .......... .......... .......... .......... 65% 18.5M 9s
174550K .......... .......... .......... .......... .......... 65% 21.3M 9s
174600K .......... .......... .......... .......... .......... 65% 14.3M 9s
174650K .......... .......... .......... .......... .......... 65% 22.8M 9s
174700K .......... .......... .......... .......... .......... 65% 13.5M 9s
174750K .......... .......... .......... .......... .......... 65% 11.7M 9s
174800K .......... .......... .......... .......... .......... 65% 16.6M 9s
174850K .......... .......... .......... .......... .......... 65% 9.67M 9s
174900K .......... .......... .......... .......... .......... 65% 9.63M 9s
174950K .......... .......... .......... .......... .......... 65% 8.25M 9s
175000K .......... .......... .......... .......... .......... 65% 12.8M 9s
175050K .......... .......... .......... .......... .......... 65% 10.3M 9s
175100K .......... .......... .......... .......... .......... 65% 8.92M 9s
175150K .......... .......... .......... .......... .......... 65% 7.56M 9s
175200K .......... .......... .......... .......... .......... 65% 11.3M 9s
175250K .......... .......... .......... .......... .......... 65% 41.2M 9s
175300K .......... .......... .......... .......... .......... 65% 27.8M 9s
175350K .......... .......... .......... .......... .......... 65% 33.4M 9s
175400K .......... .......... .......... .......... .......... 66% 46.7M 9s
175450K .......... .......... .......... .......... .......... 66% 52.2M 9s
175500K .......... .......... .......... .......... .......... 66% 38.5M 9s
175550K .......... .......... .......... .......... .......... 66% 56.9M 9s
175600K .......... .......... .......... .......... .......... 66% 43.3M 9s
175650K .......... .......... .......... .......... .......... 66% 47.1M 9s
175700K .......... .......... .......... .......... .......... 66% 43.0M 9s
175750K .......... .......... .......... .......... .......... 66% 42.3M 9s
175800K .......... .......... .......... .......... .......... 66% 16.5M 9s
175850K .......... .......... .......... .......... .......... 66% 48.9M 9s
175900K .......... .......... .......... .......... .......... 66% 79.9M 9s
175950K .......... .......... .......... .......... .......... 66% 16.6M 9s
176000K .......... .......... .......... .......... .......... 66% 9.63M 9s
176050K .......... .......... .......... .......... .......... 66% 6.00M 9s
176100K .......... .......... .......... .......... .......... 66% 9.02M 9s
176150K .......... .......... .......... .......... .......... 66% 13.3M 9s
176200K .......... .......... .......... .......... .......... 66% 9.86M 9s
176250K .......... .......... .......... .......... .......... 66% 14.4M 9s
176300K .......... .......... .......... .......... .......... 66% 12.4M 9s
176350K .......... .......... .......... .......... .......... 66% 8.64M 9s
176400K .......... .......... .......... .......... .......... 66% 12.6M 9s
176450K .......... .......... .......... .......... .......... 66% 6.17M 9s
176500K .......... .......... .......... .......... .......... 66% 9.05M 9s
176550K .......... .......... .......... .......... .......... 66% 7.96M 9s
176600K .......... .......... .......... .......... .......... 66% 5.88M 9s
176650K .......... .......... .......... .......... .......... 66% 8.17M 9s
176700K .......... .......... .......... .......... .......... 66% 6.22M 9s
176750K .......... .......... .......... .......... .......... 66% 5.13M 9s
176800K .......... .......... .......... .......... .......... 66% 8.18M 9s
176850K .......... .......... .......... .......... .......... 66% 8.65M 9s
176900K .......... .......... .......... .......... .......... 66% 10.3M 9s
176950K .......... .......... .......... .......... .......... 66% 9.54M 9s
177000K .......... .......... .......... .......... .......... 66% 10.3M 9s
177050K .......... .......... .......... .......... .......... 66% 6.01M 9s
177100K .......... .......... .......... .......... .......... 66% 4.64M 9s
177150K .......... .......... .......... .......... .......... 66% 5.18M 9s
177200K .......... .......... .......... .......... .......... 66% 7.86M 9s
177250K .......... .......... .......... .......... .......... 66% 6.71M 9s
177300K .......... .......... .......... .......... .......... 66% 6.73M 9s
177350K .......... .......... .......... .......... .......... 66% 5.07M 9s
177400K .......... .......... .......... .......... .......... 66% 8.65M 9s
177450K .......... .......... .......... .......... .......... 66% 7.33M 9s
177500K .......... .......... .......... .......... .......... 66% 5.73M 9s
177550K .......... .......... .......... .......... .......... 66% 11.8M 9s
177600K .......... .......... .......... .......... .......... 66% 11.2M 9s
177650K .......... .......... .......... .......... .......... 66% 14.8M 9s
177700K .......... .......... .......... .......... .......... 66% 9.22M 9s
177750K .......... .......... .......... .......... .......... 66% 12.0M 9s
177800K .......... .......... .......... .......... .......... 66% 12.1M 9s
177850K .......... .......... .......... .......... .......... 66% 9.56M 9s
177900K .......... .......... .......... .......... .......... 66% 10.1M 9s
177950K .......... .......... .......... .......... .......... 66% 8.47M 9s
178000K .......... .......... .......... .......... .......... 66% 10.9M 9s
178050K .......... .......... .......... .......... .......... 67% 8.26M 9s
178100K .......... .......... .......... .......... .......... 67% 8.81M 9s
178150K .......... .......... .......... .......... .......... 67% 11.6M 9s
178200K .......... .......... .......... .......... .......... 67% 8.35M 9s
178250K .......... .......... .......... .......... .......... 67% 12.7M 9s
178300K .......... .......... .......... .......... .......... 67% 14.5M 9s
178350K .......... .......... .......... .......... .......... 67% 18.3M 9s
178400K .......... .......... .......... .......... .......... 67% 49.5M 9s
178450K .......... .......... .......... .......... .......... 67% 26.0M 9s
178500K .......... .......... .......... .......... .......... 67% 17.3M 9s
178550K .......... .......... .......... .......... .......... 67% 190M 9s
178600K .......... .......... .......... .......... .......... 67% 16.2M 9s
178650K .......... .......... .......... .......... .......... 67% 22.0M 9s
178700K .......... .......... .......... .......... .......... 67% 17.2M 9s
178750K .......... .......... .......... .......... .......... 67% 17.2M 9s
178800K .......... .......... .......... .......... .......... 67% 14.6M 9s
178850K .......... .......... .......... .......... .......... 67% 11.8M 9s
178900K .......... .......... .......... .......... .......... 67% 9.68M 9s
178950K .......... .......... .......... .......... .......... 67% 10.1M 9s
179000K .......... .......... .......... .......... .......... 67% 10.0M 9s
179050K .......... .......... .......... .......... .......... 67% 6.68M 9s
179100K .......... .......... .......... .......... .......... 67% 5.94M 9s
179150K .......... .......... .......... .......... .......... 67% 6.87M 9s
179200K .......... .......... .......... .......... .......... 67% 7.16M 9s
179250K .......... .......... .......... .......... .......... 67% 7.02M 9s
179300K .......... .......... .......... .......... .......... 67% 6.80M 9s
179350K .......... .......... .......... .......... .......... 67% 20.4M 9s
179400K .......... .......... .......... .......... .......... 67% 30.6M 9s
179450K .......... .......... .......... .......... .......... 67% 18.6M 9s
179500K .......... .......... .......... .......... .......... 67% 37.8M 9s
179550K .......... .......... .......... .......... .......... 67% 78.2M 9s
179600K .......... .......... .......... .......... .......... 67% 26.5M 9s
179650K .......... .......... .......... .......... .......... 67% 44.7M 9s
179700K .......... .......... .......... .......... .......... 67% 24.7M 9s
179750K .......... .......... .......... .......... .......... 67% 42.7M 9s
179800K .......... .......... .......... .......... .......... 67% 41.0M 9s
179850K .......... .......... .......... .......... .......... 67% 40.4M 9s
179900K .......... .......... .......... .......... .......... 67% 30.2M 9s
179950K .......... .......... .......... .......... .......... 67% 27.4M 9s
180000K .......... .......... .......... .......... .......... 67% 25.0M 9s
180050K .......... .......... .......... .......... .......... 67% 48.5M 9s
180100K .......... .......... .......... .......... .......... 67% 13.8M 9s
180150K .......... .......... .......... .......... .......... 67% 219M 8s
180200K .......... .......... .......... .......... .......... 67% 14.6M 8s
180250K .......... .......... .......... .......... .......... 67% 84.8M 8s
180300K .......... .......... .......... .......... .......... 67% 30.9M 8s
180350K .......... .......... .......... .......... .......... 67% 12.2M 8s
180400K .......... .......... .......... .......... .......... 67% 11.6M 8s
180450K .......... .......... .......... .......... .......... 67% 20.5M 8s
180500K .......... .......... .......... .......... .......... 67% 15.5M 8s
180550K .......... .......... .......... .......... .......... 67% 18.1M 8s
180600K .......... .......... .......... .......... .......... 67% 14.4M 8s
180650K .......... .......... .......... .......... .......... 67% 19.5M 8s
180700K .......... .......... .......... .......... .......... 68% 14.1M 8s
180750K .......... .......... .......... .......... .......... 68% 19.4M 8s
180800K .......... .......... .......... .......... .......... 68% 9.69M 8s
180850K .......... .......... .......... .......... .......... 68% 11.5M 8s
180900K .......... .......... .......... .......... .......... 68% 12.0M 8s
180950K .......... .......... .......... .......... .......... 68% 11.1M 8s
181000K .......... .......... .......... .......... .......... 68% 16.4M 8s
181050K .......... .......... .......... .......... .......... 68% 13.4M 8s
181100K .......... .......... .......... .......... .......... 68% 15.7M 8s
181150K .......... .......... .......... .......... .......... 68% 19.5M 8s
181200K .......... .......... .......... .......... .......... 68% 10.7M 8s
181250K .......... .......... .......... .......... .......... 68% 17.6M 8s
181300K .......... .......... .......... .......... .......... 68% 16.0M 8s
181350K .......... .......... .......... .......... .......... 68% 8.43M 8s
181400K .......... .......... .......... .......... .......... 68% 23.8M 8s
181450K .......... .......... .......... .......... .......... 68% 15.6M 8s
181500K .......... .......... .......... .......... .......... 68% 14.0M 8s
181550K .......... .......... .......... .......... .......... 68% 20.4M 8s
181600K .......... .......... .......... .......... .......... 68% 15.8M 8s
181650K .......... .......... .......... .......... .......... 68% 13.2M 8s
181700K .......... .......... .......... .......... .......... 68% 10.6M 8s
181750K .......... .......... .......... .......... .......... 68% 10.7M 8s
181800K .......... .......... .......... .......... .......... 68% 9.90M 8s
181850K .......... .......... .......... .......... .......... 68% 8.51M 8s
181900K .......... .......... .......... .......... .......... 68% 17.3M 8s
181950K .......... .......... .......... .......... .......... 68% 11.3M 8s
182000K .......... .......... .......... .......... .......... 68% 12.0M 8s
182050K .......... .......... .......... .......... .......... 68% 14.8M 8s
182100K .......... .......... .......... .......... .......... 68% 8.35M 8s
182150K .......... .......... .......... .......... .......... 68% 10.5M 8s
182200K .......... .......... .......... .......... .......... 68% 6.44M 8s
182250K .......... .......... .......... .......... .......... 68% 6.55M 8s
182300K .......... .......... .......... .......... .......... 68% 14.6M 8s
182350K .......... .......... .......... .......... .......... 68% 10.5M 8s
182400K .......... .......... .......... .......... .......... 68% 13.3M 8s
182450K .......... .......... .......... .......... .......... 68% 11.5M 8s
182500K .......... .......... .......... .......... .......... 68% 12.9M 8s
182550K .......... .......... .......... .......... .......... 68% 12.8M 8s
182600K .......... .......... .......... .......... .......... 68% 12.4M 8s
182650K .......... .......... .......... .......... .......... 68% 11.5M 8s
182700K .......... .......... .......... .......... .......... 68% 9.67M 8s
182750K .......... .......... .......... .......... .......... 68% 21.8M 8s
182800K .......... .......... .......... .......... .......... 68% 12.9M 8s
182850K .......... .......... .......... .......... .......... 68% 10.0M 8s
182900K .......... .......... .......... .......... .......... 68% 12.2M 8s
182950K .......... .......... .......... .......... .......... 68% 6.85M 8s
183000K .......... .......... .......... .......... .......... 68% 10.6M 8s
183050K .......... .......... .......... .......... .......... 68% 10.3M 8s
183100K .......... .......... .......... .......... .......... 68% 7.61M 8s
183150K .......... .......... .......... .......... .......... 68% 9.37M 8s
183200K .......... .......... .......... .......... .......... 68% 9.49M 8s
183250K .......... .......... .......... .......... .......... 68% 11.8M 8s
183300K .......... .......... .......... .......... .......... 68% 9.99M 8s
183350K .......... .......... .......... .......... .......... 69% 7.65M 8s
183400K .......... .......... .......... .......... .......... 69% 7.58M 8s
183450K .......... .......... .......... .......... .......... 69% 4.75M 8s
183500K .......... .......... .......... .......... .......... 69% 9.76M 8s
183550K .......... .......... .......... .......... .......... 69% 7.25M 8s
183600K .......... .......... .......... .......... .......... 69% 6.10M 8s
183650K .......... .......... .......... .......... .......... 69% 6.56M 8s
183700K .......... .......... .......... .......... .......... 69% 6.11M 8s
183750K .......... .......... .......... .......... .......... 69% 6.01M 8s
183800K .......... .......... .......... .......... .......... 69% 8.56M 8s
183850K .......... .......... .......... .......... .......... 69% 7.14M 8s
183900K .......... .......... .......... .......... .......... 69% 6.45M 8s
183950K .......... .......... .......... .......... .......... 69% 6.76M 8s
184000K .......... .......... .......... .......... .......... 69% 6.43M 8s
184050K .......... .......... .......... .......... .......... 69% 7.64M 8s
184100K .......... .......... .......... .......... .......... 69% 5.96M 8s
184150K .......... .......... .......... .......... .......... 69% 13.3M 8s
184200K .......... .......... .......... .......... .......... 69% 11.4M 8s
184250K .......... .......... .......... .......... .......... 69% 16.1M 8s
184300K .......... .......... .......... .......... .......... 69% 12.7M 8s
184350K .......... .......... .......... .......... .......... 69% 16.7M 8s
184400K .......... .......... .......... .......... .......... 69% 19.6M 8s
184450K .......... .......... .......... .......... .......... 69% 8.98M 8s
184500K .......... .......... .......... .......... .......... 69% 36.2M 8s
184550K .......... .......... .......... .......... .......... 69% 17.4M 8s
184600K .......... .......... .......... .......... .......... 69% 13.7M 8s
184650K .......... .......... .......... .......... .......... 69% 20.2M 8s
184700K .......... .......... .......... .......... .......... 69% 8.46M 8s
184750K .......... .......... .......... .......... .......... 69% 11.8M 8s
184800K .......... .......... .......... .......... .......... 69% 8.17M 8s
184850K .......... .......... .......... .......... .......... 69% 8.39M 8s
184900K .......... .......... .......... .......... .......... 69% 8.35M 8s
184950K .......... .......... .......... .......... .......... 69% 5.77M 8s
185000K .......... .......... .......... .......... .......... 69% 7.00M 8s
185050K .......... .......... .......... .......... .......... 69% 6.61M 8s
185100K .......... .......... .......... .......... .......... 69% 7.04M 8s
185150K .......... .......... .......... .......... .......... 69% 8.20M 8s
185200K .......... .......... .......... .......... .......... 69% 6.27M 8s
185250K .......... .......... .......... .......... .......... 69% 5.55M 8s
185300K .......... .......... .......... .......... .......... 69% 9.11M 8s
185350K .......... .......... .......... .......... .......... 69% 9.74M 8s
185400K .......... .......... .......... .......... .......... 69% 12.9M 8s
185450K .......... .......... .......... .......... .......... 69% 15.7M 8s
185500K .......... .......... .......... .......... .......... 69% 18.4M 8s
185550K .......... .......... .......... .......... .......... 69% 15.1M 8s
185600K .......... .......... .......... .......... .......... 69% 13.1M 8s
185650K .......... .......... .......... .......... .......... 69% 12.6M 8s
185700K .......... .......... .......... .......... .......... 69% 8.97M 8s
185750K .......... .......... .......... .......... .......... 69% 13.1M 8s
185800K .......... .......... .......... .......... .......... 69% 12.6M 8s
185850K .......... .......... .......... .......... .......... 69% 8.46M 8s
185900K .......... .......... .......... .......... .......... 69% 11.7M 8s
185950K .......... .......... .......... .......... .......... 69% 9.75M 8s
186000K .......... .......... .......... .......... .......... 70% 10.2M 8s
186050K .......... .......... .......... .......... .......... 70% 13.1M 8s
186100K .......... .......... .......... .......... .......... 70% 8.33M 8s
186150K .......... .......... .......... .......... .......... 70% 29.6M 8s
186200K .......... .......... .......... .......... .......... 70% 14.5M 8s
186250K .......... .......... .......... .......... .......... 70% 15.2M 8s
186300K .......... .......... .......... .......... .......... 70% 12.1M 8s
186350K .......... .......... .......... .......... .......... 70% 16.7M 8s
186400K .......... .......... .......... .......... .......... 70% 11.4M 8s
186450K .......... .......... .......... .......... .......... 70% 14.3M 8s
186500K .......... .......... .......... .......... .......... 70% 11.1M 8s
186550K .......... .......... .......... .......... .......... 70% 14.1M 8s
186600K .......... .......... .......... .......... .......... 70% 11.1M 8s
186650K .......... .......... .......... .......... .......... 70% 16.1M 8s
186700K .......... .......... .......... .......... .......... 70% 24.1M 8s
186750K .......... .......... .......... .......... .......... 70% 20.2M 8s
186800K .......... .......... .......... .......... .......... 70% 13.1M 8s
186850K .......... .......... .......... .......... .......... 70% 12.1M 8s
186900K .......... .......... .......... .......... .......... 70% 19.6M 8s
186950K .......... .......... .......... .......... .......... 70% 21.1M 8s
187000K .......... .......... .......... .......... .......... 70% 16.5M 8s
187050K .......... .......... .......... .......... .......... 70% 29.1M 8s
187100K .......... .......... .......... .......... .......... 70% 8.48M 8s
187150K .......... .......... .......... .......... .......... 70% 17.4M 8s
187200K .......... .......... .......... .......... .......... 70% 10.1M 8s
187250K .......... .......... .......... .......... .......... 70% 5.36M 8s
187300K .......... .......... .......... .......... .......... 70% 121M 8s
187350K .......... .......... .......... .......... .......... 70% 13.9M 8s
187400K .......... .......... .......... .......... .......... 70% 17.8M 8s
187450K .......... .......... .......... .......... .......... 70% 10.8M 8s
187500K .......... .......... .......... .......... .......... 70% 21.1M 8s
187550K .......... .......... .......... .......... .......... 70% 16.2M 8s
187600K .......... .......... .......... .......... .......... 70% 12.7M 8s
187650K .......... .......... .......... .......... .......... 70% 14.2M 8s
187700K .......... .......... .......... .......... .......... 70% 20.4M 8s
187750K .......... .......... .......... .......... .......... 70% 6.56M 8s
187800K .......... .......... .......... .......... .......... 70% 42.3M 8s
187850K .......... .......... .......... .......... .......... 70% 6.87M 8s
187900K .......... .......... .......... .......... .......... 70% 9.51M 8s
187950K .......... .......... .......... .......... .......... 70% 8.99M 8s
188000K .......... .......... .......... .......... .......... 70% 93.3M 8s
188050K .......... .......... .......... .......... .......... 70% 10.9M 8s
188100K .......... .......... .......... .......... .......... 70% 14.3M 8s
188150K .......... .......... .......... .......... .......... 70% 14.2M 8s
188200K .......... .......... .......... .......... .......... 70% 10.5M 8s
188250K .......... .......... .......... .......... .......... 70% 8.47M 8s
188300K .......... .......... .......... .......... .......... 70% 11.3M 8s
188350K .......... .......... .......... .......... .......... 70% 7.69M 8s
188400K .......... .......... .......... .......... .......... 70% 9.48M 8s
188450K .......... .......... .......... .......... .......... 70% 9.38M 8s
188500K .......... .......... .......... .......... .......... 70% 9.32M 8s
188550K .......... .......... .......... .......... .......... 70% 6.63M 8s
188600K .......... .......... .......... .......... .......... 70% 8.99M 8s
188650K .......... .......... .......... .......... .......... 70% 7.25M 8s
188700K .......... .......... .......... .......... .......... 71% 21.8M 8s
188750K .......... .......... .......... .......... .......... 71% 19.7M 8s
188800K .......... .......... .......... .......... .......... 71% 15.2M 8s
188850K .......... .......... .......... .......... .......... 71% 9.64M 8s
188900K .......... .......... .......... .......... .......... 71% 82.9M 8s
188950K .......... .......... .......... .......... .......... 71% 8.33M 8s
189000K .......... .......... .......... .......... .......... 71% 6.11M 8s
189050K .......... .......... .......... .......... .......... 71% 21.6M 8s
189100K .......... .......... .......... .......... .......... 71% 19.5M 8s
189150K .......... .......... .......... .......... .......... 71% 13.0M 8s
189200K .......... .......... .......... .......... .......... 71% 12.9M 8s
189250K .......... .......... .......... .......... .......... 71% 30.5M 8s
189300K .......... .......... .......... .......... .......... 71% 27.5M 8s
189350K .......... .......... .......... .......... .......... 71% 17.3M 8s
189400K .......... .......... .......... .......... .......... 71% 17.9M 8s
189450K .......... .......... .......... .......... .......... 71% 14.1M 8s
189500K .......... .......... .......... .......... .......... 71% 11.4M 8s
189550K .......... .......... .......... .......... .......... 71% 9.08M 8s
189600K .......... .......... .......... .......... .......... 71% 7.94M 8s
189650K .......... .......... .......... .......... .......... 71% 7.98M 8s
189700K .......... .......... .......... .......... .......... 71% 5.76M 8s
189750K .......... .......... .......... .......... .......... 71% 7.91M 8s
189800K .......... .......... .......... .......... .......... 71% 8.29M 7s
189850K .......... .......... .......... .......... .......... 71% 6.59M 7s
189900K .......... .......... .......... .......... .......... 71% 6.69M 7s
189950K .......... .......... .......... .......... .......... 71% 11.2M 7s
190000K .......... .......... .......... .......... .......... 71% 10.7M 7s
190050K .......... .......... .......... .......... .......... 71% 12.7M 7s
190100K .......... .......... .......... .......... .......... 71% 11.3M 7s
190150K .......... .......... .......... .......... .......... 71% 13.9M 7s
190200K .......... .......... .......... .......... .......... 71% 6.17M 7s
190250K .......... .......... .......... .......... .......... 71% 5.14M 7s
190300K .......... .......... .......... .......... .......... 71% 11.6M 7s
190350K .......... .......... .......... .......... .......... 71% 8.78M 7s
190400K .......... .......... .......... .......... .......... 71% 7.85M 7s
190450K .......... .......... .......... .......... .......... 71% 8.58M 7s
190500K .......... .......... .......... .......... .......... 71% 7.44M 7s
190550K .......... .......... .......... .......... .......... 71% 6.43M 7s
190600K .......... .......... .......... .......... .......... 71% 5.00M 7s
190650K .......... .......... .......... .......... .......... 71% 7.35M 7s
190700K .......... .......... .......... .......... .......... 71% 25.2M 7s
190750K .......... .......... .......... .......... .......... 71% 8.99M 7s
190800K .......... .......... .......... .......... .......... 71% 15.1M 7s
190850K .......... .......... .......... .......... .......... 71% 37.2M 7s
190900K .......... .......... .......... .......... .......... 71% 45.3M 7s
190950K .......... .......... .......... .......... .......... 71% 24.9M 7s
191000K .......... .......... .......... .......... .......... 71% 25.9M 7s
191050K .......... .......... .......... .......... .......... 71% 46.8M 7s
191100K .......... .......... .......... .......... .......... 71% 25.0M 7s
191150K .......... .......... .......... .......... .......... 71% 16.2M 7s
191200K .......... .......... .......... .......... .......... 71% 49.1M 7s
191250K .......... .......... .......... .......... .......... 71% 14.3M 7s
191300K .......... .......... .......... .......... .......... 71% 76.2M 7s
191350K .......... .......... .......... .......... .......... 72% 16.4M 7s
191400K .......... .......... .......... .......... .......... 72% 33.6M 7s
191450K .......... .......... .......... .......... .......... 72% 19.5M 7s
191500K .......... .......... .......... .......... .......... 72% 18.5M 7s
191550K .......... .......... .......... .......... .......... 72% 11.0M 7s
191600K .......... .......... .......... .......... .......... 72% 12.5M 7s
191650K .......... .......... .......... .......... .......... 72% 13.6M 7s
191700K .......... .......... .......... .......... .......... 72% 6.31M 7s
191750K .......... .......... .......... .......... .......... 72% 12.0M 7s
191800K .......... .......... .......... .......... .......... 72% 7.69M 7s
191850K .......... .......... .......... .......... .......... 72% 6.14M 7s
191900K .......... .......... .......... .......... .......... 72% 9.37M 7s
191950K .......... .......... .......... .......... .......... 72% 7.58M 7s
192000K .......... .......... .......... .......... .......... 72% 10.5M 7s
192050K .......... .......... .......... .......... .......... 72% 9.60M 7s
192100K .......... .......... .......... .......... .......... 72% 11.1M 7s
192150K .......... .......... .......... .......... .......... 72% 13.0M 7s
192200K .......... .......... .......... .......... .......... 72% 8.87M 7s
192250K .......... .......... .......... .......... .......... 72% 6.36M 7s
192300K .......... .......... .......... .......... .......... 72% 5.58M 7s
192350K .......... .......... .......... .......... .......... 72% 8.41M 7s
192400K .......... .......... .......... .......... .......... 72% 7.06M 7s
192450K .......... .......... .......... .......... .......... 72% 9.13M 7s
192500K .......... .......... .......... .......... .......... 72% 10.6M 7s
192550K .......... .......... .......... .......... .......... 72% 5.20M 7s
192600K .......... .......... .......... .......... .......... 72% 3.71M 7s
192650K .......... .......... .......... .......... .......... 72% 5.46M 7s
192700K .......... .......... .......... .......... .......... 72% 11.9M 7s
192750K .......... .......... .......... .......... .......... 72% 8.57M 7s
192800K .......... .......... .......... .......... .......... 72% 10.2M 7s
192850K .......... .......... .......... .......... .......... 72% 13.8M 7s
192900K .......... .......... .......... .......... .......... 72% 13.9M 7s
192950K .......... .......... .......... .......... .......... 72% 11.9M 7s
193000K .......... .......... .......... .......... .......... 72% 11.4M 7s
193050K .......... .......... .......... .......... .......... 72% 11.6M 7s
193100K .......... .......... .......... .......... .......... 72% 9.55M 7s
193150K .......... .......... .......... .......... .......... 72% 10.1M 7s
193200K .......... .......... .......... .......... .......... 72% 13.7M 7s
193250K .......... .......... .......... .......... .......... 72% 13.9M 7s
193300K .......... .......... .......... .......... .......... 72% 56.5M 7s
193350K .......... .......... .......... .......... .......... 72% 31.0M 7s
193400K .......... .......... .......... .......... .......... 72% 14.1M 7s
193450K .......... .......... .......... .......... .......... 72% 14.3M 7s
193500K .......... .......... .......... .......... .......... 72% 23.4M 7s
193550K .......... .......... .......... .......... .......... 72% 8.93M 7s
193600K .......... .......... .......... .......... .......... 72% 10.9M 7s
193650K .......... .......... .......... .......... .......... 72% 8.89M 7s
193700K .......... .......... .......... .......... .......... 72% 9.80M 7s
193750K .......... .......... .......... .......... .......... 72% 9.20M 7s
193800K .......... .......... .......... .......... .......... 72% 8.53M 7s
193850K .......... .......... .......... .......... .......... 72% 6.23M 7s
193900K .......... .......... .......... .......... .......... 72% 6.89M 7s
193950K .......... .......... .......... .......... .......... 72% 5.49M 7s
194000K .......... .......... .......... .......... .......... 73% 6.49M 7s
194050K .......... .......... .......... .......... .......... 73% 6.40M 7s
194100K .......... .......... .......... .......... .......... 73% 23.1M 7s
194150K .......... .......... .......... .......... .......... 73% 13.8M 7s
194200K .......... .......... .......... .......... .......... 73% 13.0M 7s
194250K .......... .......... .......... .......... .......... 73% 16.3M 7s
194300K .......... .......... .......... .......... .......... 73% 14.5M 7s
194350K .......... .......... .......... .......... .......... 73% 16.8M 7s
194400K .......... .......... .......... .......... .......... 73% 13.6M 7s
194450K .......... .......... .......... .......... .......... 73% 11.8M 7s
194500K .......... .......... .......... .......... .......... 73% 11.8M 7s
194550K .......... .......... .......... .......... .......... 73% 13.1M 7s
194600K .......... .......... .......... .......... .......... 73% 9.82M 7s
194650K .......... .......... .......... .......... .......... 73% 8.41M 7s
194700K .......... .......... .......... .......... .......... 73% 9.03M 7s
194750K .......... .......... .......... .......... .......... 73% 10.4M 7s
194800K .......... .......... .......... .......... .......... 73% 9.70M 7s
194850K .......... .......... .......... .......... .......... 73% 7.86M 7s
194900K .......... .......... .......... .......... .......... 73% 15.6M 7s
194950K .......... .......... .......... .......... .......... 73% 23.9M 7s
195000K .......... .......... .......... .......... .......... 73% 19.7M 7s
195050K .......... .......... .......... .......... .......... 73% 19.6M 7s
195100K .......... .......... .......... .......... .......... 73% 15.8M 7s
195150K .......... .......... .......... .......... .......... 73% 9.45M 7s
195200K .......... .......... .......... .......... .......... 73% 34.7M 7s
195250K .......... .......... .......... .......... .......... 73% 13.2M 7s
195300K .......... .......... .......... .......... .......... 73% 15.8M 7s
195350K .......... .......... .......... .......... .......... 73% 8.91M 7s
195400K .......... .......... .......... .......... .......... 73% 6.20M 7s
195450K .......... .......... .......... .......... .......... 73% 4.82M 7s
195500K .......... .......... .......... .......... .......... 73% 5.28M 7s
195550K .......... .......... .......... .......... .......... 73% 4.65M 7s
195600K .......... .......... .......... .......... .......... 73% 4.86M 7s
195650K .......... .......... .......... .......... .......... 73% 5.16M 7s
195700K .......... .......... .......... .......... .......... 73% 6.46M 7s
195750K .......... .......... .......... .......... .......... 73% 5.30M 7s
195800K .......... .......... .......... .......... .......... 73% 6.52M 7s
195850K .......... .......... .......... .......... .......... 73% 7.64M 7s
195900K .......... .......... .......... .......... .......... 73% 6.47M 7s
195950K .......... .......... .......... .......... .......... 73% 6.09M 7s
196000K .......... .......... .......... .......... .......... 73% 8.91M 7s
196050K .......... .......... .......... .......... .......... 73% 20.9M 7s
196100K .......... .......... .......... .......... .......... 73% 26.0M 7s
196150K .......... .......... .......... .......... .......... 73% 34.4M 7s
196200K .......... .......... .......... .......... .......... 73% 22.6M 7s
196250K .......... .......... .......... .......... .......... 73% 20.3M 7s
196300K .......... .......... .......... .......... .......... 73% 17.9M 7s
196350K .......... .......... .......... .......... .......... 73% 12.9M 7s
196400K .......... .......... .......... .......... .......... 73% 17.5M 7s
196450K .......... .......... .......... .......... .......... 73% 18.3M 7s
196500K .......... .......... .......... .......... .......... 73% 21.4M 7s
196550K .......... .......... .......... .......... .......... 73% 19.1M 7s
196600K .......... .......... .......... .......... .......... 73% 10.5M 7s
196650K .......... .......... .......... .......... .......... 74% 7.01M 7s
196700K .......... .......... .......... .......... .......... 74% 5.78M 7s
196750K .......... .......... .......... .......... .......... 74% 10.5M 7s
196800K .......... .......... .......... .......... .......... 74% 4.77M 7s
196850K .......... .......... .......... .......... .......... 74% 3.15M 7s
196900K .......... .......... .......... .......... .......... 74% 4.37M 7s
196950K .......... .......... .......... .......... .......... 74% 7.98M 7s
197000K .......... .......... .......... .......... .......... 74% 6.96M 7s
197050K .......... .......... .......... .......... .......... 74% 7.82M 7s
197100K .......... .......... .......... .......... .......... 74% 7.21M 7s
197150K .......... .......... .......... .......... .......... 74% 6.32M 7s
197200K .......... .......... .......... .......... .......... 74% 6.83M 7s
197250K .......... .......... .......... .......... .......... 74% 12.4M 7s
197300K .......... .......... .......... .......... .......... 74% 10.3M 7s
197350K .......... .......... .......... .......... .......... 74% 10.5M 7s
197400K .......... .......... .......... .......... .......... 74% 9.49M 7s
197450K .......... .......... .......... .......... .......... 74% 7.64M 7s
197500K .......... .......... .......... .......... .......... 74% 9.27M 7s
197550K .......... .......... .......... .......... .......... 74% 10.0M 7s
197600K .......... .......... .......... .......... .......... 74% 8.93M 7s
197650K .......... .......... .......... .......... .......... 74% 8.84M 7s
197700K .......... .......... .......... .......... .......... 74% 5.10M 7s
197750K .......... .......... .......... .......... .......... 74% 6.70M 7s
197800K .......... .......... .......... .......... .......... 74% 7.22M 7s
197850K .......... .......... .......... .......... .......... 74% 5.72M 7s
197900K .......... .......... .......... .......... .......... 74% 7.61M 7s
197950K .......... .......... .......... .......... .......... 74% 16.0M 7s
198000K .......... .......... .......... .......... .......... 74% 12.3M 7s
198050K .......... .......... .......... .......... .......... 74% 33.2M 7s
198100K .......... .......... .......... .......... .......... 74% 19.1M 7s
198150K .......... .......... .......... .......... .......... 74% 11.9M 7s
198200K .......... .......... .......... .......... .......... 74% 13.7M 7s
198250K .......... .......... .......... .......... .......... 74% 11.2M 7s
198300K .......... .......... .......... .......... .......... 74% 12.7M 7s
198350K .......... .......... .......... .......... .......... 74% 10.3M 7s
198400K .......... .......... .......... .......... .......... 74% 12.5M 7s
198450K .......... .......... .......... .......... .......... 74% 9.34M 7s
198500K .......... .......... .......... .......... .......... 74% 10.6M 7s
198550K .......... .......... .......... .......... .......... 74% 12.6M 7s
198600K .......... .......... .......... .......... .......... 74% 9.63M 7s
198650K .......... .......... .......... .......... .......... 74% 11.7M 7s
198700K .......... .......... .......... .......... .......... 74% 7.89M 7s
198750K .......... .......... .......... .......... .......... 74% 7.76M 7s
198800K .......... .......... .......... .......... .......... 74% 7.72M 7s
198850K .......... .......... .......... .......... .......... 74% 6.52M 7s
198900K .......... .......... .......... .......... .......... 74% 7.41M 7s
198950K .......... .......... .......... .......... .......... 74% 8.70M 7s
199000K .......... .......... .......... .......... .......... 74% 28.2M 7s
199050K .......... .......... .......... .......... .......... 74% 34.3M 7s
199100K .......... .......... .......... .......... .......... 74% 14.5M 7s
199150K .......... .......... .......... .......... .......... 74% 40.9M 7s
199200K .......... .......... .......... .......... .......... 74% 22.0M 7s
199250K .......... .......... .......... .......... .......... 74% 20.6M 7s
199300K .......... .......... .......... .......... .......... 75% 19.9M 7s
199350K .......... .......... .......... .......... .......... 75% 18.2M 7s
199400K .......... .......... .......... .......... .......... 75% 15.1M 7s
199450K .......... .......... .......... .......... .......... 75% 14.3M 7s
199500K .......... .......... .......... .......... .......... 75% 21.3M 7s
199550K .......... .......... .......... .......... .......... 75% 15.0M 7s
199600K .......... .......... .......... .......... .......... 75% 13.6M 7s
199650K .......... .......... .......... .......... .......... 75% 12.6M 7s
199700K .......... .......... .......... .......... .......... 75% 9.49M 7s
199750K .......... .......... .......... .......... .......... 75% 10.2M 7s
199800K .......... .......... .......... .......... .......... 75% 9.65M 7s
199850K .......... .......... .......... .......... .......... 75% 7.27M 7s
199900K .......... .......... .......... .......... .......... 75% 8.68M 7s
199950K .......... .......... .......... .......... .......... 75% 4.53M 7s
200000K .......... .......... .......... .......... .......... 75% 5.66M 6s
200050K .......... .......... .......... .......... .......... 75% 6.39M 6s
200100K .......... .......... .......... .......... .......... 75% 4.90M 6s
200150K .......... .......... .......... .......... .......... 75% 3.70M 6s
200200K .......... .......... .......... .......... .......... 75% 2.73M 6s
200250K .......... .......... .......... .......... .......... 75% 7.54M 6s
200300K .......... .......... .......... .......... .......... 75% 18.8M 6s
200350K .......... .......... .......... .......... .......... 75% 8.39M 6s
200400K .......... .......... .......... .......... .......... 75% 8.90M 6s
200450K .......... .......... .......... .......... .......... 75% 9.64M 6s
200500K .......... .......... .......... .......... .......... 75% 8.07M 6s
200550K .......... .......... .......... .......... .......... 75% 6.92M 6s
200600K .......... .......... .......... .......... .......... 75% 7.39M 6s
200650K .......... .......... .......... .......... .......... 75% 8.72M 6s
200700K .......... .......... .......... .......... .......... 75% 7.22M 6s
200750K .......... .......... .......... .......... .......... 75% 10.4M 6s
200800K .......... .......... .......... .......... .......... 75% 8.45M 6s
200850K .......... .......... .......... .......... .......... 75% 12.6M 6s
200900K .......... .......... .......... .......... .......... 75% 15.1M 6s
200950K .......... .......... .......... .......... .......... 75% 22.7M 6s
201000K .......... .......... .......... .......... .......... 75% 22.5M 6s
201050K .......... .......... .......... .......... .......... 75% 15.4M 6s
201100K .......... .......... .......... .......... .......... 75% 35.9M 6s
201150K .......... .......... .......... .......... .......... 75% 10.9M 6s
201200K .......... .......... .......... .......... .......... 75% 24.9M 6s
201250K .......... .......... .......... .......... .......... 75% 10.2M 6s
201300K .......... .......... .......... .......... .......... 75% 21.6M 6s
201350K .......... .......... .......... .......... .......... 75% 12.3M 6s
201400K .......... .......... .......... .......... .......... 75% 15.1M 6s
201450K .......... .......... .......... .......... .......... 75% 12.7M 6s
201500K .......... .......... .......... .......... .......... 75% 15.4M 6s
201550K .......... .......... .......... .......... .......... 75% 13.3M 6s
201600K .......... .......... .......... .......... .......... 75% 13.2M 6s
201650K .......... .......... .......... .......... .......... 75% 13.3M 6s
201700K .......... .......... .......... .......... .......... 75% 11.4M 6s
201750K .......... .......... .......... .......... .......... 75% 8.42M 6s
201800K .......... .......... .......... .......... .......... 75% 9.62M 6s
201850K .......... .......... .......... .......... .......... 75% 9.39M 6s
201900K .......... .......... .......... .......... .......... 75% 10.4M 6s
201950K .......... .......... .......... .......... .......... 76% 8.76M 6s
202000K .......... .......... .......... .......... .......... 76% 6.12M 6s
202050K .......... .......... .......... .......... .......... 76% 6.91M 6s
202100K .......... .......... .......... .......... .......... 76% 13.4M 6s
202150K .......... .......... .......... .......... .......... 76% 12.2M 6s
202200K .......... .......... .......... .......... .......... 76% 12.8M 6s
202250K .......... .......... .......... .......... .......... 76% 14.5M 6s
202300K .......... .......... .......... .......... .......... 76% 14.6M 6s
202350K .......... .......... .......... .......... .......... 76% 10.4M 6s
202400K .......... .......... .......... .......... .......... 76% 10.2M 6s
202450K .......... .......... .......... .......... .......... 76% 7.29M 6s
202500K .......... .......... .......... .......... .......... 76% 7.68M 6s
202550K .......... .......... .......... .......... .......... 76% 9.62M 6s
202600K .......... .......... .......... .......... .......... 76% 7.38M 6s
202650K .......... .......... .......... .......... .......... 76% 7.93M 6s
202700K .......... .......... .......... .......... .......... 76% 11.4M 6s
202750K .......... .......... .......... .......... .......... 76% 17.8M 6s
202800K .......... .......... .......... .......... .......... 76% 95.7M 6s
202850K .......... .......... .......... .......... .......... 76% 30.0M 6s
202900K .......... .......... .......... .......... .......... 76% 18.5M 6s
202950K .......... .......... .......... .......... .......... 76% 20.5M 6s
203000K .......... .......... .......... .......... .......... 76% 62.2M 6s
203050K .......... .......... .......... .......... .......... 76% 23.5M 6s
203100K .......... .......... .......... .......... .......... 76% 21.6M 6s
203150K .......... .......... .......... .......... .......... 76% 22.3M 6s
203200K .......... .......... .......... .......... .......... 76% 18.9M 6s
203250K .......... .......... .......... .......... .......... 76% 19.3M 6s
203300K .......... .......... .......... .......... .......... 76% 32.0M 6s
203350K .......... .......... .......... .......... .......... 76% 17.2M 6s
203400K .......... .......... .......... .......... .......... 76% 34.4M 6s
203450K .......... .......... .......... .......... .......... 76% 15.0M 6s
203500K .......... .......... .......... .......... .......... 76% 24.2M 6s
203550K .......... .......... .......... .......... .......... 76% 21.1M 6s
203600K .......... .......... .......... .......... .......... 76% 13.1M 6s
203650K .......... .......... .......... .......... .......... 76% 20.6M 6s
203700K .......... .......... .......... .......... .......... 76% 7.88M 6s
203750K .......... .......... .......... .......... .......... 76% 14.4M 6s
203800K .......... .......... .......... .......... .......... 76% 9.47M 6s
203850K .......... .......... .......... .......... .......... 76% 9.44M 6s
203900K .......... .......... .......... .......... .......... 76% 9.15M 6s
203950K .......... .......... .......... .......... .......... 76% 6.37M 6s
204000K .......... .......... .......... .......... .......... 76% 8.53M 6s
204050K .......... .......... .......... .......... .......... 76% 6.56M 6s
204100K .......... .......... .......... .......... .......... 76% 6.50M 6s
204150K .......... .......... .......... .......... .......... 76% 7.49M 6s
204200K .......... .......... .......... .......... .......... 76% 6.17M 6s
204250K .......... .......... .......... .......... .......... 76% 8.05M 6s
204300K .......... .......... .......... .......... .......... 76% 7.56M 6s
204350K .......... .......... .......... .......... .......... 76% 9.14M 6s
204400K .......... .......... .......... .......... .......... 76% 15.4M 6s
204450K .......... .......... .......... .......... .......... 76% 15.1M 6s
204500K .......... .......... .......... .......... .......... 76% 20.3M 6s
204550K .......... .......... .......... .......... .......... 76% 16.6M 6s
204600K .......... .......... .......... .......... .......... 76% 14.3M 6s
204650K .......... .......... .......... .......... .......... 77% 15.2M 6s
204700K .......... .......... .......... .......... .......... 77% 11.9M 6s
204750K .......... .......... .......... .......... .......... 77% 9.81M 6s
204800K .......... .......... .......... .......... .......... 77% 11.0M 6s
204850K .......... .......... .......... .......... .......... 77% 9.27M 6s
204900K .......... .......... .......... .......... .......... 77% 10.5M 6s
204950K .......... .......... .......... .......... .......... 77% 9.51M 6s
205000K .......... .......... .......... .......... .......... 77% 10.6M 6s
205050K .......... .......... .......... .......... .......... 77% 14.2M 6s
205100K .......... .......... .......... .......... .......... 77% 18.7M 6s
205150K .......... .......... .......... .......... .......... 77% 17.9M 6s
205200K .......... .......... .......... .......... .......... 77% 44.2M 6s
205250K .......... .......... .......... .......... .......... 77% 25.0M 6s
205300K .......... .......... .......... .......... .......... 77% 18.4M 6s
205350K .......... .......... .......... .......... .......... 77% 18.7M 6s
205400K .......... .......... .......... .......... .......... 77% 16.7M 6s
205450K .......... .......... .......... .......... .......... 77% 18.8M 6s
205500K .......... .......... .......... .......... .......... 77% 18.2M 6s
205550K .......... .......... .......... .......... .......... 77% 13.6M 6s
205600K .......... .......... .......... .......... .......... 77% 12.2M 6s
205650K .......... .......... .......... .......... .......... 77% 16.7M 6s
205700K .......... .......... .......... .......... .......... 77% 14.0M 6s
205750K .......... .......... .......... .......... .......... 77% 12.1M 6s
205800K .......... .......... .......... .......... .......... 77% 8.97M 6s
205850K .......... .......... .......... .......... .......... 77% 10.8M 6s
205900K .......... .......... .......... .......... .......... 77% 11.5M 6s
205950K .......... .......... .......... .......... .......... 77% 10.7M 6s
206000K .......... .......... .......... .......... .......... 77% 11.7M 6s
206050K .......... .......... .......... .......... .......... 77% 8.40M 6s
206100K .......... .......... .......... .......... .......... 77% 9.45M 6s
206150K .......... .......... .......... .......... .......... 77% 8.07M 6s
206200K .......... .......... .......... .......... .......... 77% 6.62M 6s
206250K .......... .......... .......... .......... .......... 77% 7.03M 6s
206300K .......... .......... .......... .......... .......... 77% 8.39M 6s
206350K .......... .......... .......... .......... .......... 77% 6.42M 6s
206400K .......... .......... .......... .......... .......... 77% 9.81M 6s
206450K .......... .......... .......... .......... .......... 77% 9.66M 6s
206500K .......... .......... .......... .......... .......... 77% 10.1M 6s
206550K .......... .......... .......... .......... .......... 77% 10.0M 6s
206600K .......... .......... .......... .......... .......... 77% 10.1M 6s
206650K .......... .......... .......... .......... .......... 77% 11.0M 6s
206700K .......... .......... .......... .......... .......... 77% 12.0M 6s
206750K .......... .......... .......... .......... .......... 77% 15.8M 6s
206800K .......... .......... .......... .......... .......... 77% 31.8M 6s
206850K .......... .......... .......... .......... .......... 77% 15.6M 6s
206900K .......... .......... .......... .......... .......... 77% 29.3M 6s
206950K .......... .......... .......... .......... .......... 77% 15.0M 6s
207000K .......... .......... .......... .......... .......... 77% 34.9M 6s
207050K .......... .......... .......... .......... .......... 77% 18.7M 6s
207100K .......... .......... .......... .......... .......... 77% 16.6M 6s
207150K .......... .......... .......... .......... .......... 77% 19.3M 6s
207200K .......... .......... .......... .......... .......... 77% 14.9M 6s
207250K .......... .......... .......... .......... .......... 77% 21.6M 6s
207300K .......... .......... .......... .......... .......... 78% 15.4M 6s
207350K .......... .......... .......... .......... .......... 78% 20.7M 6s
207400K .......... .......... .......... .......... .......... 78% 18.2M 6s
207450K .......... .......... .......... .......... .......... 78% 13.7M 6s
207500K .......... .......... .......... .......... .......... 78% 16.7M 6s
207550K .......... .......... .......... .......... .......... 78% 15.8M 6s
207600K .......... .......... .......... .......... .......... 78% 19.5M 6s
207650K .......... .......... .......... .......... .......... 78% 15.7M 6s
207700K .......... .......... .......... .......... .......... 78% 15.7M 6s
207750K .......... .......... .......... .......... .......... 78% 12.5M 6s
207800K .......... .......... .......... .......... .......... 78% 15.0M 6s
207850K .......... .......... .......... .......... .......... 78% 9.20M 6s
207900K .......... .......... .......... .......... .......... 78% 7.52M 6s
207950K .......... .......... .......... .......... .......... 78% 6.78M 6s
208000K .......... .......... .......... .......... .......... 78% 11.9M 6s
208050K .......... .......... .......... .......... .......... 78% 15.5M 6s
208100K .......... .......... .......... .......... .......... 78% 15.8M 6s
208150K .......... .......... .......... .......... .......... 78% 22.5M 6s
208200K .......... .......... .......... .......... .......... 78% 13.3M 6s
208250K .......... .......... .......... .......... .......... 78% 12.3M 6s
208300K .......... .......... .......... .......... .......... 78% 19.8M 6s
208350K .......... .......... .......... .......... .......... 78% 9.56M 6s
208400K .......... .......... .......... .......... .......... 78% 21.0M 6s
208450K .......... .......... .......... .......... .......... 78% 12.1M 6s
208500K .......... .......... .......... .......... .......... 78% 15.8M 6s
208550K .......... .......... .......... .......... .......... 78% 8.39M 6s
208600K .......... .......... .......... .......... .......... 78% 13.0M 6s
208650K .......... .......... .......... .......... .......... 78% 9.21M 6s
208700K .......... .......... .......... .......... .......... 78% 7.54M 6s
208750K .......... .......... .......... .......... .......... 78% 8.33M 6s
208800K .......... .......... .......... .......... .......... 78% 6.90M 6s
208850K .......... .......... .......... .......... .......... 78% 7.61M 6s
208900K .......... .......... .......... .......... .......... 78% 8.56M 6s
208950K .......... .......... .......... .......... .......... 78% 10.6M 6s
209000K .......... .......... .......... .......... .......... 78% 10.6M 6s
209050K .......... .......... .......... .......... .......... 78% 12.0M 6s
209100K .......... .......... .......... .......... .......... 78% 6.27M 6s
209150K .......... .......... .......... .......... .......... 78% 11.3M 6s
209200K .......... .......... .......... .......... .......... 78% 6.73M 6s
209250K .......... .......... .......... .......... .......... 78% 9.96M 6s
209300K .......... .......... .......... .......... .......... 78% 9.98M 6s
209350K .......... .......... .......... .......... .......... 78% 10.4M 6s
209400K .......... .......... .......... .......... .......... 78% 8.41M 6s
209450K .......... .......... .......... .......... .......... 78% 7.04M 6s
209500K .......... .......... .......... .......... .......... 78% 10.4M 6s
209550K .......... .......... .......... .......... .......... 78% 6.99M 6s
209600K .......... .......... .......... .......... .......... 78% 11.9M 6s
209650K .......... .......... .......... .......... .......... 78% 16.1M 6s
209700K .......... .......... .......... .......... .......... 78% 12.2M 6s
209750K .......... .......... .......... .......... .......... 78% 13.7M 6s
209800K .......... .......... .......... .......... .......... 78% 15.2M 5s
209850K .......... .......... .......... .......... .......... 78% 12.9M 5s
209900K .......... .......... .......... .......... .......... 78% 13.5M 5s
209950K .......... .......... .......... .......... .......... 79% 7.45M 5s
210000K .......... .......... .......... .......... .......... 79% 13.4M 5s
210050K .......... .......... .......... .......... .......... 79% 10.3M 5s
210100K .......... .......... .......... .......... .......... 79% 13.7M 5s
210150K .......... .......... .......... .......... .......... 79% 19.7M 5s
210200K .......... .......... .......... .......... .......... 79% 13.0M 5s
210250K .......... .......... .......... .......... .......... 79% 16.8M 5s
210300K .......... .......... .......... .......... .......... 79% 14.9M 5s
210350K .......... .......... .......... .......... .......... 79% 16.2M 5s
210400K .......... .......... .......... .......... .......... 79% 16.4M 5s
210450K .......... .......... .......... .......... .......... 79% 13.6M 5s
210500K .......... .......... .......... .......... .......... 79% 17.0M 5s
210550K .......... .......... .......... .......... .......... 79% 16.8M 5s
210600K .......... .......... .......... .......... .......... 79% 15.2M 5s
210650K .......... .......... .......... .......... .......... 79% 24.9M 5s
210700K .......... .......... .......... .......... .......... 79% 20.3M 5s
210750K .......... .......... .......... .......... .......... 79% 26.8M 5s
210800K .......... .......... .......... .......... .......... 79% 19.0M 5s
210850K .......... .......... .......... .......... .......... 79% 16.7M 5s
210900K .......... .......... .......... .......... .......... 79% 13.6M 5s
210950K .......... .......... .......... .......... .......... 79% 15.0M 5s
211000K .......... .......... .......... .......... .......... 79% 16.0M 5s
211050K .......... .......... .......... .......... .......... 79% 13.2M 5s
211100K .......... .......... .......... .......... .......... 79% 9.98M 5s
211150K .......... .......... .......... .......... .......... 79% 8.71M 5s
211200K .......... .......... .......... .......... .......... 79% 5.68M 5s
211250K .......... .......... .......... .......... .......... 79% 6.64M 5s
211300K .......... .......... .......... .......... .......... 79% 7.02M 5s
211350K .......... .......... .......... .......... .......... 79% 7.20M 5s
211400K .......... .......... .......... .......... .......... 79% 10.1M 5s
211450K .......... .......... .......... .......... .......... 79% 13.0M 5s
211500K .......... .......... .......... .......... .......... 79% 15.0M 5s
211550K .......... .......... .......... .......... .......... 79% 18.6M 5s
211600K .......... .......... .......... .......... .......... 79% 16.1M 5s
211650K .......... .......... .......... .......... .......... 79% 20.0M 5s
211700K .......... .......... .......... .......... .......... 79% 15.3M 5s
211750K .......... .......... .......... .......... .......... 79% 19.6M 5s
211800K .......... .......... .......... .......... .......... 79% 15.4M 5s
211850K .......... .......... .......... .......... .......... 79% 18.4M 5s
211900K .......... .......... .......... .......... .......... 79% 11.9M 5s
211950K .......... .......... .......... .......... .......... 79% 13.0M 5s
212000K .......... .......... .......... .......... .......... 79% 28.6M 5s
212050K .......... .......... .......... .......... .......... 79% 17.0M 5s
212100K .......... .......... .......... .......... .......... 79% 14.0M 5s
212150K .......... .......... .......... .......... .......... 79% 21.0M 5s
212200K .......... .......... .......... .......... .......... 79% 14.9M 5s
212250K .......... .......... .......... .......... .......... 79% 13.7M 5s
212300K .......... .......... .......... .......... .......... 79% 12.6M 5s
212350K .......... .......... .......... .......... .......... 79% 12.2M 5s
212400K .......... .......... .......... .......... .......... 79% 13.9M 5s
212450K .......... .......... .......... .......... .......... 79% 13.3M 5s
212500K .......... .......... .......... .......... .......... 79% 8.14M 5s
212550K .......... .......... .......... .......... .......... 79% 10.3M 5s
212600K .......... .......... .......... .......... .......... 80% 11.1M 5s
212650K .......... .......... .......... .......... .......... 80% 8.68M 5s
212700K .......... .......... .......... .......... .......... 80% 8.82M 5s
212750K .......... .......... .......... .......... .......... 80% 11.7M 5s
212800K .......... .......... .......... .......... .......... 80% 11.8M 5s
212850K .......... .......... .......... .......... .......... 80% 8.30M 5s
212900K .......... .......... .......... .......... .......... 80% 8.61M 5s
212950K .......... .......... .......... .......... .......... 80% 12.1M 5s
213000K .......... .......... .......... .......... .......... 80% 9.92M 5s
213050K .......... .......... .......... .......... .......... 80% 11.8M 5s
213100K .......... .......... .......... .......... .......... 80% 18.3M 5s
213150K .......... .......... .......... .......... .......... 80% 14.1M 5s
213200K .......... .......... .......... .......... .......... 80% 15.4M 5s
213250K .......... .......... .......... .......... .......... 80% 13.7M 5s
213300K .......... .......... .......... .......... .......... 80% 13.8M 5s
213350K .......... .......... .......... .......... .......... 80% 9.68M 5s
213400K .......... .......... .......... .......... .......... 80% 12.0M 5s
213450K .......... .......... .......... .......... .......... 80% 11.1M 5s
213500K .......... .......... .......... .......... .......... 80% 12.3M 5s
213550K .......... .......... .......... .......... .......... 80% 14.9M 5s
213600K .......... .......... .......... .......... .......... 80% 13.7M 5s
213650K .......... .......... .......... .......... .......... 80% 16.1M 5s
213700K .......... .......... .......... .......... .......... 80% 14.0M 5s
213750K .......... .......... .......... .......... .......... 80% 14.6M 5s
213800K .......... .......... .......... .......... .......... 80% 16.8M 5s
213850K .......... .......... .......... .......... .......... 80% 13.6M 5s
213900K .......... .......... .......... .......... .......... 80% 14.8M 5s
213950K .......... .......... .......... .......... .......... 80% 14.5M 5s
214000K .......... .......... .......... .......... .......... 80% 17.3M 5s
214050K .......... .......... .......... .......... .......... 80% 12.1M 5s
214100K .......... .......... .......... .......... .......... 80% 11.0M 5s
214150K .......... .......... .......... .......... .......... 80% 29.2M 5s
214200K .......... .......... .......... .......... .......... 80% 9.62M 5s
214250K .......... .......... .......... .......... .......... 80% 13.3M 5s
214300K .......... .......... .......... .......... .......... 80% 10.2M 5s
214350K .......... .......... .......... .......... .......... 80% 8.18M 5s
214400K .......... .......... .......... .......... .......... 80% 11.0M 5s
214450K .......... .......... .......... .......... .......... 80% 13.2M 5s
214500K .......... .......... .......... .......... .......... 80% 13.0M 5s
214550K .......... .......... .......... .......... .......... 80% 15.0M 5s
214600K .......... .......... .......... .......... .......... 80% 5.39M 5s
214650K .......... .......... .......... .......... .......... 80% 8.11M 5s
214700K .......... .......... .......... .......... .......... 80% 7.67M 5s
214750K .......... .......... .......... .......... .......... 80% 11.0M 5s
214800K .......... .......... .......... .......... .......... 80% 9.73M 5s
214850K .......... .......... .......... .......... .......... 80% 7.45M 5s
214900K .......... .......... .......... .......... .......... 80% 8.41M 5s
214950K .......... .......... .......... .......... .......... 80% 6.04M 5s
215000K .......... .......... .......... .......... .......... 80% 8.42M 5s
215050K .......... .......... .......... .......... .......... 80% 8.26M 5s
215100K .......... .......... .......... .......... .......... 80% 8.37M 5s
215150K .......... .......... .......... .......... .......... 80% 8.47M 5s
215200K .......... .......... .......... .......... .......... 80% 6.05M 5s
215250K .......... .......... .......... .......... .......... 81% 6.59M 5s
215300K .......... .......... .......... .......... .......... 81% 7.51M 5s
215350K .......... .......... .......... .......... .......... 81% 6.40M 5s
215400K .......... .......... .......... .......... .......... 81% 8.30M 5s
215450K .......... .......... .......... .......... .......... 81% 7.37M 5s
215500K .......... .......... .......... .......... .......... 81% 33.1M 5s
215550K .......... .......... .......... .......... .......... 81% 18.5M 5s
215600K .......... .......... .......... .......... .......... 81% 13.0M 5s
215650K .......... .......... .......... .......... .......... 81% 9.93M 5s
215700K .......... .......... .......... .......... .......... 81% 13.1M 5s
215750K .......... .......... .......... .......... .......... 81% 8.13M 5s
215800K .......... .......... .......... .......... .......... 81% 7.46M 5s
215850K .......... .......... .......... .......... .......... 81% 8.71M 5s
215900K .......... .......... .......... .......... .......... 81% 7.87M 5s
215950K .......... .......... .......... .......... .......... 81% 8.21M 5s
216000K .......... .......... .......... .......... .......... 81% 8.21M 5s
216050K .......... .......... .......... .......... .......... 81% 11.5M 5s
216100K .......... .......... .......... .......... .......... 81% 9.36M 5s
216150K .......... .......... .......... .......... .......... 81% 29.4M 5s
216200K .......... .......... .......... .......... .......... 81% 35.9M 5s
216250K .......... .......... .......... .......... .......... 81% 26.5M 5s
216300K .......... .......... .......... .......... .......... 81% 16.7M 5s
216350K .......... .......... .......... .......... .......... 81% 75.9M 5s
216400K .......... .......... .......... .......... .......... 81% 17.2M 5s
216450K .......... .......... .......... .......... .......... 81% 25.0M 5s
216500K .......... .......... .......... .......... .......... 81% 30.2M 5s
216550K .......... .......... .......... .......... .......... 81% 20.9M 5s
216600K .......... .......... .......... .......... .......... 81% 12.9M 5s
216650K .......... .......... .......... .......... .......... 81% 20.0M 5s
216700K .......... .......... .......... .......... .......... 81% 9.40M 5s
216750K .......... .......... .......... .......... .......... 81% 9.67M 5s
216800K .......... .......... .......... .......... .......... 81% 13.2M 5s
216850K .......... .......... .......... .......... .......... 81% 9.05M 5s
216900K .......... .......... .......... .......... .......... 81% 18.1M 5s
216950K .......... .......... .......... .......... .......... 81% 11.4M 5s
217000K .......... .......... .......... .......... .......... 81% 13.0M 5s
217050K .......... .......... .......... .......... .......... 81% 14.2M 5s
217100K .......... .......... .......... .......... .......... 81% 8.66M 5s
217150K .......... .......... .......... .......... .......... 81% 10.3M 5s
217200K .......... .......... .......... .......... .......... 81% 6.58M 5s
217250K .......... .......... .......... .......... .......... 81% 10.6M 5s
217300K .......... .......... .......... .......... .......... 81% 8.74M 5s
217350K .......... .......... .......... .......... .......... 81% 6.75M 5s
217400K .......... .......... .......... .......... .......... 81% 6.75M 5s
217450K .......... .......... .......... .......... .......... 81% 6.99M 5s
217500K .......... .......... .......... .......... .......... 81% 8.99M 5s
217550K .......... .......... .......... .......... .......... 81% 8.38M 5s
217600K .......... .......... .......... .......... .......... 81% 8.50M 5s
217650K .......... .......... .......... .......... .......... 81% 30.5M 5s
217700K .......... .......... .......... .......... .......... 81% 16.2M 5s
217750K .......... .......... .......... .......... .......... 81% 81.1M 5s
217800K .......... .......... .......... .......... .......... 81% 44.3M 5s
217850K .......... .......... .......... .......... .......... 81% 24.5M 5s
217900K .......... .......... .......... .......... .......... 82% 28.1M 5s
217950K .......... .......... .......... .......... .......... 82% 24.3M 5s
218000K .......... .......... .......... .......... .......... 82% 27.7M 5s
218050K .......... .......... .......... .......... .......... 82% 22.4M 5s
218100K .......... .......... .......... .......... .......... 82% 20.3M 5s
218150K .......... .......... .......... .......... .......... 82% 15.1M 5s
218200K .......... .......... .......... .......... .......... 82% 26.4M 5s
218250K .......... .......... .......... .......... .......... 82% 18.9M 5s
218300K .......... .......... .......... .......... .......... 82% 19.3M 5s
218350K .......... .......... .......... .......... .......... 82% 10.2M 5s
218400K .......... .......... .......... .......... .......... 82% 18.4M 5s
218450K .......... .......... .......... .......... .......... 82% 8.86M 5s
218500K .......... .......... .......... .......... .......... 82% 15.7M 5s
218550K .......... .......... .......... .......... .......... 82% 15.7M 5s
218600K .......... .......... .......... .......... .......... 82% 10.8M 5s
218650K .......... .......... .......... .......... .......... 82% 10.0M 5s
218700K .......... .......... .......... .......... .......... 82% 9.29M 5s
218750K .......... .......... .......... .......... .......... 82% 6.66M 5s
218800K .......... .......... .......... .......... .......... 82% 11.3M 5s
218850K .......... .......... .......... .......... .......... 82% 10.3M 5s
218900K .......... .......... .......... .......... .......... 82% 11.9M 5s
218950K .......... .......... .......... .......... .......... 82% 9.83M 5s
219000K .......... .......... .......... .......... .......... 82% 7.62M 5s
219050K .......... .......... .......... .......... .......... 82% 15.0M 5s
219100K .......... .......... .......... .......... .......... 82% 8.29M 5s
219150K .......... .......... .......... .......... .......... 82% 8.33M 5s
219200K .......... .......... .......... .......... .......... 82% 8.10M 5s
219250K .......... .......... .......... .......... .......... 82% 7.55M 5s
219300K .......... .......... .......... .......... .......... 82% 5.39M 5s
219350K .......... .......... .......... .......... .......... 82% 5.47M 5s
219400K .......... .......... .......... .......... .......... 82% 6.23M 5s
219450K .......... .......... .......... .......... .......... 82% 6.22M 5s
219500K .......... .......... .......... .......... .......... 82% 6.54M 5s
219550K .......... .......... .......... .......... .......... 82% 4.85M 5s
219600K .......... .......... .......... .......... .......... 82% 3.78M 5s
219650K .......... .......... .......... .......... .......... 82% 5.26M 5s
219700K .......... .......... .......... .......... .......... 82% 5.98M 5s
219750K .......... .......... .......... .......... .......... 82% 6.83M 4s
219800K .......... .......... .......... .......... .......... 82% 6.70M 4s
219850K .......... .......... .......... .......... .......... 82% 6.03M 4s
219900K .......... .......... .......... .......... .......... 82% 9.14M 4s
219950K .......... .......... .......... .......... .......... 82% 6.51M 4s
220000K .......... .......... .......... .......... .......... 82% 6.01M 4s
220050K .......... .......... .......... .......... .......... 82% 6.24M 4s
220100K .......... .......... .......... .......... .......... 82% 4.15M 4s
220150K .......... .......... .......... .......... .......... 82% 3.35M 4s
220200K .......... .......... .......... .......... .......... 82% 3.22M 4s
220250K .......... .......... .......... .......... .......... 82% 1.62M 4s
220300K .......... .......... .......... .......... .......... 82% 6.21M 4s
220350K .......... .......... .......... .......... .......... 82% 6.65M 4s
220400K .......... .......... .......... .......... .......... 82% 7.22M 4s
220450K .......... .......... .......... .......... .......... 82% 6.04M 4s
220500K .......... .......... .......... .......... .......... 82% 22.0M 4s
220550K .......... .......... .......... .......... .......... 83% 23.8M 4s
220600K .......... .......... .......... .......... .......... 83% 19.5M 4s
220650K .......... .......... .......... .......... .......... 83% 43.8M 4s
220700K .......... .......... .......... .......... .......... 83% 29.6M 4s
220750K .......... .......... .......... .......... .......... 83% 16.4M 4s
220800K .......... .......... .......... .......... .......... 83% 16.0M 4s
220850K .......... .......... .......... .......... .......... 83% 38.0M 4s
220900K .......... .......... .......... .......... .......... 83% 11.0M 4s
220950K .......... .......... .......... .......... .......... 83% 17.5M 4s
221000K .......... .......... .......... .......... .......... 83% 11.7M 4s
221050K .......... .......... .......... .......... .......... 83% 8.18M 4s
221100K .......... .......... .......... .......... .......... 83% 7.01M 4s
221150K .......... .......... .......... .......... .......... 83% 6.37M 4s
221200K .......... .......... .......... .......... .......... 83% 5.02M 4s
221250K .......... .......... .......... .......... .......... 83% 9.39M 4s
221300K .......... .......... .......... .......... .......... 83% 7.85M 4s
221350K .......... .......... .......... .......... .......... 83% 5.55M 4s
221400K .......... .......... .......... .......... .......... 83% 7.31M 4s
221450K .......... .......... .......... .......... .......... 83% 4.22M 4s
221500K .......... .......... .......... .......... .......... 83% 4.23M 4s
221550K .......... .......... .......... .......... .......... 83% 3.75M 4s
221600K .......... .......... .......... .......... .......... 83% 2.64M 4s
221650K .......... .......... .......... .......... .......... 83% 9.24M 4s
221700K .......... .......... .......... .......... .......... 83% 17.4M 4s
221750K .......... .......... .......... .......... .......... 83% 24.6M 4s
221800K .......... .......... .......... .......... .......... 83% 22.4M 4s
221850K .......... .......... .......... .......... .......... 83% 13.8M 4s
221900K .......... .......... .......... .......... .......... 83% 19.3M 4s
221950K .......... .......... .......... .......... .......... 83% 19.4M 4s
222000K .......... .......... .......... .......... .......... 83% 20.3M 4s
222050K .......... .......... .......... .......... .......... 83% 19.5M 4s
222100K .......... .......... .......... .......... .......... 83% 18.2M 4s
222150K .......... .......... .......... .......... .......... 83% 17.0M 4s
222200K .......... .......... .......... .......... .......... 83% 9.45M 4s
222250K .......... .......... .......... .......... .......... 83% 26.0M 4s
222300K .......... .......... .......... .......... .......... 83% 12.0M 4s
222350K .......... .......... .......... .......... .......... 83% 13.5M 4s
222400K .......... .......... .......... .......... .......... 83% 13.9M 4s
222450K .......... .......... .......... .......... .......... 83% 12.6M 4s
222500K .......... .......... .......... .......... .......... 83% 19.5M 4s
222550K .......... .......... .......... .......... .......... 83% 14.3M 4s
222600K .......... .......... .......... .......... .......... 83% 12.5M 4s
222650K .......... .......... .......... .......... .......... 83% 17.4M 4s
222700K .......... .......... .......... .......... .......... 83% 13.9M 4s
222750K .......... .......... .......... .......... .......... 83% 12.3M 4s
222800K .......... .......... .......... .......... .......... 83% 15.7M 4s
222850K .......... .......... .......... .......... .......... 83% 14.8M 4s
222900K .......... .......... .......... .......... .......... 83% 17.9M 4s
222950K .......... .......... .......... .......... .......... 83% 17.1M 4s
223000K .......... .......... .......... .......... .......... 83% 18.5M 4s
223050K .......... .......... .......... .......... .......... 83% 13.2M 4s
223100K .......... .......... .......... .......... .......... 83% 15.1M 4s
223150K .......... .......... .......... .......... .......... 83% 21.5M 4s
223200K .......... .......... .......... .......... .......... 83% 18.0M 4s
223250K .......... .......... .......... .......... .......... 84% 20.7M 4s
223300K .......... .......... .......... .......... .......... 84% 13.3M 4s
223350K .......... .......... .......... .......... .......... 84% 12.0M 4s
223400K .......... .......... .......... .......... .......... 84% 13.5M 4s
223450K .......... .......... .......... .......... .......... 84% 9.22M 4s
223500K .......... .......... .......... .......... .......... 84% 11.4M 4s
223550K .......... .......... .......... .......... .......... 84% 11.1M 4s
223600K .......... .......... .......... .......... .......... 84% 12.5M 4s
223650K .......... .......... .......... .......... .......... 84% 8.82M 4s
223700K .......... .......... .......... .......... .......... 84% 13.8M 4s
223750K .......... .......... .......... .......... .......... 84% 15.4M 4s
223800K .......... .......... .......... .......... .......... 84% 15.6M 4s
223850K .......... .......... .......... .......... .......... 84% 13.8M 4s
223900K .......... .......... .......... .......... .......... 84% 15.5M 4s
223950K .......... .......... .......... .......... .......... 84% 11.8M 4s
224000K .......... .......... .......... .......... .......... 84% 12.0M 4s
224050K .......... .......... .......... .......... .......... 84% 17.3M 4s
224100K .......... .......... .......... .......... .......... 84% 25.6M 4s
224150K .......... .......... .......... .......... .......... 84% 22.3M 4s
224200K .......... .......... .......... .......... .......... 84% 15.2M 4s
224250K .......... .......... .......... .......... .......... 84% 15.7M 4s
224300K .......... .......... .......... .......... .......... 84% 16.7M 4s
224350K .......... .......... .......... .......... .......... 84% 9.21M 4s
224400K .......... .......... .......... .......... .......... 84% 10.1M 4s
224450K .......... .......... .......... .......... .......... 84% 11.5M 4s
224500K .......... .......... .......... .......... .......... 84% 10.3M 4s
224550K .......... .......... .......... .......... .......... 84% 9.43M 4s
224600K .......... .......... .......... .......... .......... 84% 7.18M 4s
224650K .......... .......... .......... .......... .......... 84% 7.39M 4s
224700K .......... .......... .......... .......... .......... 84% 8.06M 4s
224750K .......... .......... .......... .......... .......... 84% 9.16M 4s
224800K .......... .......... .......... .......... .......... 84% 12.0M 4s
224850K .......... .......... .......... .......... .......... 84% 9.32M 4s
224900K .......... .......... .......... .......... .......... 84% 11.5M 4s
224950K .......... .......... .......... .......... .......... 84% 9.06M 4s
225000K .......... .......... .......... .......... .......... 84% 24.1M 4s
225050K .......... .......... .......... .......... .......... 84% 18.7M 4s
225100K .......... .......... .......... .......... .......... 84% 23.1M 4s
225150K .......... .......... .......... .......... .......... 84% 47.0M 4s
225200K .......... .......... .......... .......... .......... 84% 18.3M 4s
225250K .......... .......... .......... .......... .......... 84% 23.3M 4s
225300K .......... .......... .......... .......... .......... 84% 23.4M 4s
225350K .......... .......... .......... .......... .......... 84% 18.0M 4s
225400K .......... .......... .......... .......... .......... 84% 22.4M 4s
225450K .......... .......... .......... .......... .......... 84% 13.1M 4s
225500K .......... .......... .......... .......... .......... 84% 17.0M 4s
225550K .......... .......... .......... .......... .......... 84% 12.9M 4s
225600K .......... .......... .......... .......... .......... 84% 16.2M 4s
225650K .......... .......... .......... .......... .......... 84% 22.9M 4s
225700K .......... .......... .......... .......... .......... 84% 18.9M 4s
225750K .......... .......... .......... .......... .......... 84% 28.4M 4s
225800K .......... .......... .......... .......... .......... 84% 16.4M 4s
225850K .......... .......... .......... .......... .......... 84% 10.6M 4s
225900K .......... .......... .......... .......... .......... 85% 14.9M 4s
225950K .......... .......... .......... .......... .......... 85% 14.2M 4s
226000K .......... .......... .......... .......... .......... 85% 23.1M 4s
226050K .......... .......... .......... .......... .......... 85% 15.9M 4s
226100K .......... .......... .......... .......... .......... 85% 18.6M 4s
226150K .......... .......... .......... .......... .......... 85% 19.9M 4s
226200K .......... .......... .......... .......... .......... 85% 19.1M 4s
226250K .......... .......... .......... .......... .......... 85% 22.8M 4s
226300K .......... .......... .......... .......... .......... 85% 25.6M 4s
226350K .......... .......... .......... .......... .......... 85% 21.7M 4s
226400K .......... .......... .......... .......... .......... 85% 15.2M 4s
226450K .......... .......... .......... .......... .......... 85% 7.61M 4s
226500K .......... .......... .......... .......... .......... 85% 6.03M 4s
226550K .......... .......... .......... .......... .......... 85% 8.94M 4s
226600K .......... .......... .......... .......... .......... 85% 7.91M 4s
226650K .......... .......... .......... .......... .......... 85% 6.85M 4s
226700K .......... .......... .......... .......... .......... 85% 12.2M 4s
226750K .......... .......... .......... .......... .......... 85% 19.8M 4s
226800K .......... .......... .......... .......... .......... 85% 12.6M 4s
226850K .......... .......... .......... .......... .......... 85% 15.8M 4s
226900K .......... .......... .......... .......... .......... 85% 34.8M 4s
226950K .......... .......... .......... .......... .......... 85% 13.9M 4s
227000K .......... .......... .......... .......... .......... 85% 16.4M 4s
227050K .......... .......... .......... .......... .......... 85% 15.7M 4s
227100K .......... .......... .......... .......... .......... 85% 13.6M 4s
227150K .......... .......... .......... .......... .......... 85% 17.6M 4s
227200K .......... .......... .......... .......... .......... 85% 15.5M 4s
227250K .......... .......... .......... .......... .......... 85% 21.1M 4s
227300K .......... .......... .......... .......... .......... 85% 14.3M 4s
227350K .......... .......... .......... .......... .......... 85% 17.1M 4s
227400K .......... .......... .......... .......... .......... 85% 25.0M 4s
227450K .......... .......... .......... .......... .......... 85% 21.5M 4s
227500K .......... .......... .......... .......... .......... 85% 19.3M 4s
227550K .......... .......... .......... .......... .......... 85% 21.8M 4s
227600K .......... .......... .......... .......... .......... 85% 22.2M 4s
227650K .......... .......... .......... .......... .......... 85% 20.6M 4s
227700K .......... .......... .......... .......... .......... 85% 19.1M 4s
227750K .......... .......... .......... .......... .......... 85% 17.9M 4s
227800K .......... .......... .......... .......... .......... 85% 5.77M 4s
227850K .......... .......... .......... .......... .......... 85% 89.4M 4s
227900K .......... .......... .......... .......... .......... 85% 8.83M 4s
227950K .......... .......... .......... .......... .......... 85% 81.6M 4s
228000K .......... .......... .......... .......... .......... 85% 113M 4s
228050K .......... .......... .......... .......... .......... 85% 15.4M 4s
228100K .......... .......... .......... .......... .......... 85% 26.0M 4s
228150K .......... .......... .......... .......... .......... 85% 37.3M 4s
228200K .......... .......... .......... .......... .......... 85% 49.5M 4s
228250K .......... .......... .......... .......... .......... 85% 31.1M 4s
228300K .......... .......... .......... .......... .......... 85% 44.0M 4s
228350K .......... .......... .......... .......... .......... 85% 18.8M 4s
228400K .......... .......... .......... .......... .......... 85% 34.1M 4s
228450K .......... .......... .......... .......... .......... 85% 18.2M 4s
228500K .......... .......... .......... .......... .......... 85% 20.8M 4s
228550K .......... .......... .......... .......... .......... 86% 18.8M 4s
228600K .......... .......... .......... .......... .......... 86% 11.7M 4s
228650K .......... .......... .......... .......... .......... 86% 15.4M 4s
228700K .......... .......... .......... .......... .......... 86% 16.1M 4s
228750K .......... .......... .......... .......... .......... 86% 17.5M 4s
228800K .......... .......... .......... .......... .......... 86% 19.8M 4s
228850K .......... .......... .......... .......... .......... 86% 14.5M 4s
228900K .......... .......... .......... .......... .......... 86% 16.9M 4s
228950K .......... .......... .......... .......... .......... 86% 15.8M 4s
229000K .......... .......... .......... .......... .......... 86% 19.6M 4s
229050K .......... .......... .......... .......... .......... 86% 16.5M 4s
229100K .......... .......... .......... .......... .......... 86% 8.66M 4s
229150K .......... .......... .......... .......... .......... 86% 14.4M 4s
229200K .......... .......... .......... .......... .......... 86% 15.6M 4s
229250K .......... .......... .......... .......... .......... 86% 20.3M 4s
229300K .......... .......... .......... .......... .......... 86% 18.4M 4s
229350K .......... .......... .......... .......... .......... 86% 11.9M 4s
229400K .......... .......... .......... .......... .......... 86% 19.4M 4s
229450K .......... .......... .......... .......... .......... 86% 11.8M 4s
229500K .......... .......... .......... .......... .......... 86% 16.2M 4s
229550K .......... .......... .......... .......... .......... 86% 18.7M 4s
229600K .......... .......... .......... .......... .......... 86% 16.0M 4s
229650K .......... .......... .......... .......... .......... 86% 20.6M 4s
229700K .......... .......... .......... .......... .......... 86% 16.4M 4s
229750K .......... .......... .......... .......... .......... 86% 16.3M 3s
229800K .......... .......... .......... .......... .......... 86% 17.6M 3s
229850K .......... .......... .......... .......... .......... 86% 12.8M 3s
229900K .......... .......... .......... .......... .......... 86% 21.4M 3s
229950K .......... .......... .......... .......... .......... 86% 16.0M 3s
230000K .......... .......... .......... .......... .......... 86% 15.5M 3s
230050K .......... .......... .......... .......... .......... 86% 11.8M 3s
230100K .......... .......... .......... .......... .......... 86% 10.8M 3s
230150K .......... .......... .......... .......... .......... 86% 15.6M 3s
230200K .......... .......... .......... .......... .......... 86% 11.7M 3s
230250K .......... .......... .......... .......... .......... 86% 15.1M 3s
230300K .......... .......... .......... .......... .......... 86% 10.7M 3s
230350K .......... .......... .......... .......... .......... 86% 12.4M 3s
230400K .......... .......... .......... .......... .......... 86% 20.8M 3s
230450K .......... .......... .......... .......... .......... 86% 14.7M 3s
230500K .......... .......... .......... .......... .......... 86% 15.9M 3s
230550K .......... .......... .......... .......... .......... 86% 17.6M 3s
230600K .......... .......... .......... .......... .......... 86% 13.8M 3s
230650K .......... .......... .......... .......... .......... 86% 16.9M 3s
230700K .......... .......... .......... .......... .......... 86% 15.7M 3s
230750K .......... .......... .......... .......... .......... 86% 18.0M 3s
230800K .......... .......... .......... .......... .......... 86% 14.7M 3s
230850K .......... .......... .......... .......... .......... 86% 9.37M 3s
230900K .......... .......... .......... .......... .......... 86% 15.8M 3s
230950K .......... .......... .......... .......... .......... 86% 12.6M 3s
231000K .......... .......... .......... .......... .......... 86% 17.5M 3s
231050K .......... .......... .......... .......... .......... 86% 14.7M 3s
231100K .......... .......... .......... .......... .......... 86% 11.7M 3s
231150K .......... .......... .......... .......... .......... 86% 16.3M 3s
231200K .......... .......... .......... .......... .......... 87% 13.3M 3s
231250K .......... .......... .......... .......... .......... 87% 17.4M 3s
231300K .......... .......... .......... .......... .......... 87% 11.8M 3s
231350K .......... .......... .......... .......... .......... 87% 9.52M 3s
231400K .......... .......... .......... .......... .......... 87% 10.3M 3s
231450K .......... .......... .......... .......... .......... 87% 8.93M 3s
231500K .......... .......... .......... .......... .......... 87% 12.7M 3s
231550K .......... .......... .......... .......... .......... 87% 11.4M 3s
231600K .......... .......... .......... .......... .......... 87% 9.87M 3s
231650K .......... .......... .......... .......... .......... 87% 11.4M 3s
231700K .......... .......... .......... .......... .......... 87% 7.10M 3s
231750K .......... .......... .......... .......... .......... 87% 17.4M 3s
231800K .......... .......... .......... .......... .......... 87% 16.2M 3s
231850K .......... .......... .......... .......... .......... 87% 13.5M 3s
231900K .......... .......... .......... .......... .......... 87% 9.71M 3s
231950K .......... .......... .......... .......... .......... 87% 23.5M 3s
232000K .......... .......... .......... .......... .......... 87% 22.5M 3s
232050K .......... .......... .......... .......... .......... 87% 18.7M 3s
232100K .......... .......... .......... .......... .......... 87% 10.7M 3s
232150K .......... .......... .......... .......... .......... 87% 13.9M 3s
232200K .......... .......... .......... .......... .......... 87% 5.96M 3s
232250K .......... .......... .......... .......... .......... 87% 17.0M 3s
232300K .......... .......... .......... .......... .......... 87% 12.3M 3s
232350K .......... .......... .......... .......... .......... 87% 12.4M 3s
232400K .......... .......... .......... .......... .......... 87% 15.5M 3s
232450K .......... .......... .......... .......... .......... 87% 9.23M 3s
232500K .......... .......... .......... .......... .......... 87% 121M 3s
232550K .......... .......... .......... .......... .......... 87% 11.4M 3s
232600K .......... .......... .......... .......... .......... 87% 11.7M 3s
232650K .......... .......... .......... .......... .......... 87% 10.4M 3s
232700K .......... .......... .......... .......... .......... 87% 3.97M 3s
232750K .......... .......... .......... .......... .......... 87% 6.12M 3s
232800K .......... .......... .......... .......... .......... 87% 4.09M 3s
232850K .......... .......... .......... .......... .......... 87% 4.11M 3s
232900K .......... .......... .......... .......... .......... 87% 5.56M 3s
232950K .......... .......... .......... .......... .......... 87% 13.1M 3s
233000K .......... .......... .......... .......... .......... 87% 14.5M 3s
233050K .......... .......... .......... .......... .......... 87% 13.8M 3s
233100K .......... .......... .......... .......... .......... 87% 10.0M 3s
233150K .......... .......... .......... .......... .......... 87% 8.16M 3s
233200K .......... .......... .......... .......... .......... 87% 16.9M 3s
233250K .......... .......... .......... .......... .......... 87% 11.7M 3s
233300K .......... .......... .......... .......... .......... 87% 11.1M 3s
233350K .......... .......... .......... .......... .......... 87% 7.72M 3s
233400K .......... .......... .......... .......... .......... 87% 11.6M 3s
233450K .......... .......... .......... .......... .......... 87% 5.81M 3s
233500K .......... .......... .......... .......... .......... 87% 7.74M 3s
233550K .......... .......... .......... .......... .......... 87% 12.0M 3s
233600K .......... .......... .......... .......... .......... 87% 7.07M 3s
233650K .......... .......... .......... .......... .......... 87% 15.4M 3s
233700K .......... .......... .......... .......... .......... 87% 16.3M 3s
233750K .......... .......... .......... .......... .......... 87% 21.3M 3s
233800K .......... .......... .......... .......... .......... 87% 14.2M 3s
233850K .......... .......... .......... .......... .......... 88% 10.3M 3s
233900K .......... .......... .......... .......... .......... 88% 23.4M 3s
233950K .......... .......... .......... .......... .......... 88% 9.94M 3s
234000K .......... .......... .......... .......... .......... 88% 8.94M 3s
234050K .......... .......... .......... .......... .......... 88% 7.75M 3s
234100K .......... .......... .......... .......... .......... 88% 8.14M 3s
234150K .......... .......... .......... .......... .......... 88% 8.05M 3s
234200K .......... .......... .......... .......... .......... 88% 6.60M 3s
234250K .......... .......... .......... .......... .......... 88% 7.90M 3s
234300K .......... .......... .......... .......... .......... 88% 12.2M 3s
234350K .......... .......... .......... .......... .......... 88% 7.91M 3s
234400K .......... .......... .......... .......... .......... 88% 8.63M 3s
234450K .......... .......... .......... .......... .......... 88% 14.1M 3s
234500K .......... .......... .......... .......... .......... 88% 14.5M 3s
234550K .......... .......... .......... .......... .......... 88% 14.2M 3s
234600K .......... .......... .......... .......... .......... 88% 16.3M 3s
234650K .......... .......... .......... .......... .......... 88% 16.2M 3s
234700K .......... .......... .......... .......... .......... 88% 6.60M 3s
234750K .......... .......... .......... .......... .......... 88% 5.87M 3s
234800K .......... .......... .......... .......... .......... 88% 163M 3s
234850K .......... .......... .......... .......... .......... 88% 12.2M 3s
234900K .......... .......... .......... .......... .......... 88% 20.4M 3s
234950K .......... .......... .......... .......... .......... 88% 8.80M 3s
235000K .......... .......... .......... .......... .......... 88% 12.1M 3s
235050K .......... .......... .......... .......... .......... 88% 7.30M 3s
235100K .......... .......... .......... .......... .......... 88% 50.9M 3s
235150K .......... .......... .......... .......... .......... 88% 3.95M 3s
235200K .......... .......... .......... .......... .......... 88% 131M 3s
235250K .......... .......... .......... .......... .......... 88% 9.23M 3s
235300K .......... .......... .......... .......... .......... 88% 34.1M 3s
235350K .......... .......... .......... .......... .......... 88% 9.73M 3s
235400K .......... .......... .......... .......... .......... 88% 16.4M 3s
235450K .......... .......... .......... .......... .......... 88% 17.1M 3s
235500K .......... .......... .......... .......... .......... 88% 12.5M 3s
235550K .......... .......... .......... .......... .......... 88% 25.3M 3s
235600K .......... .......... .......... .......... .......... 88% 30.6M 3s
235650K .......... .......... .......... .......... .......... 88% 18.0M 3s
235700K .......... .......... .......... .......... .......... 88% 10.4M 3s
235750K .......... .......... .......... .......... .......... 88% 15.1M 3s
235800K .......... .......... .......... .......... .......... 88% 11.0M 3s
235850K .......... .......... .......... .......... .......... 88% 19.4M 3s
235900K .......... .......... .......... .......... .......... 88% 17.1M 3s
235950K .......... .......... .......... .......... .......... 88% 4.17M 3s
236000K .......... .......... .......... .......... .......... 88% 80.5M 3s
236050K .......... .......... .......... .......... .......... 88% 15.5M 3s
236100K .......... .......... .......... .......... .......... 88% 8.51M 3s
236150K .......... .......... .......... .......... .......... 88% 21.8M 3s
236200K .......... .......... .......... .......... .......... 88% 12.3M 3s
236250K .......... .......... .......... .......... .......... 88% 12.7M 3s
236300K .......... .......... .......... .......... .......... 88% 20.7M 3s
236350K .......... .......... .......... .......... .......... 88% 14.3M 3s
236400K .......... .......... .......... .......... .......... 88% 14.2M 3s
236450K .......... .......... .......... .......... .......... 88% 8.06M 3s
236500K .......... .......... .......... .......... .......... 89% 10.1M 3s
236550K .......... .......... .......... .......... .......... 89% 7.50M 3s
236600K .......... .......... .......... .......... .......... 89% 1.79M 3s
236650K .......... .......... .......... .......... .......... 89% 1.83M 3s
236700K .......... .......... .......... .......... .......... 89% 3.48M 3s
236750K .......... .......... .......... .......... .......... 89% 4.84M 3s
236800K .......... .......... .......... .......... .......... 89% 3.76M 3s
236850K .......... .......... .......... .......... .......... 89% 3.20M 3s
236900K .......... .......... .......... .......... .......... 89% 4.52M 3s
236950K .......... .......... .......... .......... .......... 89% 3.31M 3s
237000K .......... .......... .......... .......... .......... 89% 4.04M 3s
237050K .......... .......... .......... .......... .......... 89% 4.03M 3s
237100K .......... .......... .......... .......... .......... 89% 2.95M 3s
237150K .......... .......... .......... .......... .......... 89% 3.75M 3s
237200K .......... .......... .......... .......... .......... 89% 3.21M 3s
237250K .......... .......... .......... .......... .......... 89% 4.83M 3s
237300K .......... .......... .......... .......... .......... 89% 4.15M 3s
237350K .......... .......... .......... .......... .......... 89% 3.98M 3s
237400K .......... .......... .......... .......... .......... 89% 4.09M 3s
237450K .......... .......... .......... .......... .......... 89% 2.54M 3s
237500K .......... .......... .......... .......... .......... 89% 12.8M 3s
237550K .......... .......... .......... .......... .......... 89% 35.9M 3s
237600K .......... .......... .......... .......... .......... 89% 14.1M 3s
237650K .......... .......... .......... .......... .......... 89% 26.6M 3s
237700K .......... .......... .......... .......... .......... 89% 58.0M 3s
237750K .......... .......... .......... .......... .......... 89% 8.81M 3s
237800K .......... .......... .......... .......... .......... 89% 219M 3s
237850K .......... .......... .......... .......... .......... 89% 74.5M 3s
237900K .......... .......... .......... .......... .......... 89% 25.1M 3s
237950K .......... .......... .......... .......... .......... 89% 12.9M 3s
238000K .......... .......... .......... .......... .......... 89% 29.5M 3s
238050K .......... .......... .......... .......... .......... 89% 13.8M 3s
238100K .......... .......... .......... .......... .......... 89% 14.5M 3s
238150K .......... .......... .......... .......... .......... 89% 4.01M 3s
238200K .......... .......... .......... .......... .......... 89% 4.58M 3s
238250K .......... .......... .......... .......... .......... 89% 104M 3s
238300K .......... .......... .......... .......... .......... 89% 4.15M 3s
238350K .......... .......... .......... .......... .......... 89% 4.51M 3s
238400K .......... .......... .......... .......... .......... 89% 4.46M 3s
238450K .......... .......... .......... .......... .......... 89% 98.3M 3s
238500K .......... .......... .......... .......... .......... 89% 4.14M 3s
238550K .......... .......... .......... .......... .......... 89% 83.7M 3s
238600K .......... .......... .......... .......... .......... 89% 4.18M 3s
238650K .......... .......... .......... .......... .......... 89% 4.66M 3s
238700K .......... .......... .......... .......... .......... 89% 45.0M 3s
238750K .......... .......... .......... .......... .......... 89% 46.3M 3s
238800K .......... .......... .......... .......... .......... 89% 4.84M 3s
238850K .......... .......... .......... .......... .......... 89% 53.5M 3s
238900K .......... .......... .......... .......... .......... 89% 27.0M 3s
238950K .......... .......... .......... .......... .......... 89% 16.6M 3s
239000K .......... .......... .......... .......... .......... 89% 17.6M 3s
239050K .......... .......... .......... .......... .......... 89% 22.4M 3s
239100K .......... .......... .......... .......... .......... 89% 17.5M 3s
239150K .......... .......... .......... .......... .......... 89% 18.2M 3s
239200K .......... .......... .......... .......... .......... 90% 14.7M 3s
239250K .......... .......... .......... .......... .......... 90% 25.0M 3s
239300K .......... .......... .......... .......... .......... 90% 18.9M 3s
239350K .......... .......... .......... .......... .......... 90% 21.6M 3s
239400K .......... .......... .......... .......... .......... 90% 17.2M 3s
239450K .......... .......... .......... .......... .......... 90% 21.5M 3s
239500K .......... .......... .......... .......... .......... 90% 13.6M 3s
239550K .......... .......... .......... .......... .......... 90% 18.2M 3s
239600K .......... .......... .......... .......... .......... 90% 12.3M 3s
239650K .......... .......... .......... .......... .......... 90% 15.4M 3s
239700K .......... .......... .......... .......... .......... 90% 11.9M 3s
239750K .......... .......... .......... .......... .......... 90% 9.98M 3s
239800K .......... .......... .......... .......... .......... 90% 7.52M 3s
239850K .......... .......... .......... .......... .......... 90% 6.26M 3s
239900K .......... .......... .......... .......... .......... 90% 7.45M 3s
239950K .......... .......... .......... .......... .......... 90% 4.33M 3s
240000K .......... .......... .......... .......... .......... 90% 6.85M 3s
240050K .......... .......... .......... .......... .......... 90% 5.42M 3s
240100K .......... .......... .......... .......... .......... 90% 4.07M 3s
240150K .......... .......... .......... .......... .......... 90% 7.73M 2s
240200K .......... .......... .......... .......... .......... 90% 8.31M 2s
240250K .......... .......... .......... .......... .......... 90% 10.6M 2s
240300K .......... .......... .......... .......... .......... 90% 14.9M 2s
240350K .......... .......... .......... .......... .......... 90% 16.3M 2s
240400K .......... .......... .......... .......... .......... 90% 16.0M 2s
240450K .......... .......... .......... .......... .......... 90% 13.7M 2s
240500K .......... .......... .......... .......... .......... 90% 16.4M 2s
240550K .......... .......... .......... .......... .......... 90% 9.48M 2s
240600K .......... .......... .......... .......... .......... 90% 9.69M 2s
240650K .......... .......... .......... .......... .......... 90% 14.1M 2s
240700K .......... .......... .......... .......... .......... 90% 10.6M 2s
240750K .......... .......... .......... .......... .......... 90% 12.5M 2s
240800K .......... .......... .......... .......... .......... 90% 6.24M 2s
240850K .......... .......... .......... .......... .......... 90% 5.89M 2s
240900K .......... .......... .......... .......... .......... 90% 6.46M 2s
240950K .......... .......... .......... .......... .......... 90% 6.16M 2s
241000K .......... .......... .......... .......... .......... 90% 5.22M 2s
241050K .......... .......... .......... .......... .......... 90% 5.14M 2s
241100K .......... .......... .......... .......... .......... 90% 4.88M 2s
241150K .......... .......... .......... .......... .......... 90% 5.43M 2s
241200K .......... .......... .......... .......... .......... 90% 3.72M 2s
241250K .......... .......... .......... .......... .......... 90% 4.95M 2s
241300K .......... .......... .......... .......... .......... 90% 5.72M 2s
241350K .......... .......... .......... .......... .......... 90% 13.3M 2s
241400K .......... .......... .......... .......... .......... 90% 44.9M 2s
241450K .......... .......... .......... .......... .......... 90% 20.4M 2s
241500K .......... .......... .......... .......... .......... 90% 20.2M 2s
241550K .......... .......... .......... .......... .......... 90% 19.7M 2s
241600K .......... .......... .......... .......... .......... 90% 18.4M 2s
241650K .......... .......... .......... .......... .......... 90% 19.2M 2s
241700K .......... .......... .......... .......... .......... 90% 12.5M 2s
241750K .......... .......... .......... .......... .......... 90% 10.7M 2s
241800K .......... .......... .......... .......... .......... 90% 24.4M 2s
241850K .......... .......... .......... .......... .......... 91% 10.3M 2s
241900K .......... .......... .......... .......... .......... 91% 17.2M 2s
241950K .......... .......... .......... .......... .......... 91% 12.7M 2s
242000K .......... .......... .......... .......... .......... 91% 13.4M 2s
242050K .......... .......... .......... .......... .......... 91% 11.4M 2s
242100K .......... .......... .......... .......... .......... 91% 9.10M 2s
242150K .......... .......... .......... .......... .......... 91% 10.2M 2s
242200K .......... .......... .......... .......... .......... 91% 9.41M 2s
242250K .......... .......... .......... .......... .......... 91% 11.9M 2s
242300K .......... .......... .......... .......... .......... 91% 9.68M 2s
242350K .......... .......... .......... .......... .......... 91% 14.4M 2s
242400K .......... .......... .......... .......... .......... 91% 17.3M 2s
242450K .......... .......... .......... .......... .......... 91% 11.4M 2s
242500K .......... .......... .......... .......... .......... 91% 14.5M 2s
242550K .......... .......... .......... .......... .......... 91% 16.9M 2s
242600K .......... .......... .......... .......... .......... 91% 9.58M 2s
242650K .......... .......... .......... .......... .......... 91% 14.8M 2s
242700K .......... .......... .......... .......... .......... 91% 15.4M 2s
242750K .......... .......... .......... .......... .......... 91% 12.2M 2s
242800K .......... .......... .......... .......... .......... 91% 15.9M 2s
242850K .......... .......... .......... .......... .......... 91% 16.5M 2s
242900K .......... .......... .......... .......... .......... 91% 17.5M 2s
242950K .......... .......... .......... .......... .......... 91% 13.3M 2s
243000K .......... .......... .......... .......... .......... 91% 14.0M 2s
243050K .......... .......... .......... .......... .......... 91% 17.4M 2s
243100K .......... .......... .......... .......... .......... 91% 9.22M 2s
243150K .......... .......... .......... .......... .......... 91% 16.1M 2s
243200K .......... .......... .......... .......... .......... 91% 12.2M 2s
243250K .......... .......... .......... .......... .......... 91% 15.4M 2s
243300K .......... .......... .......... .......... .......... 91% 13.3M 2s
243350K .......... .......... .......... .......... .......... 91% 6.99M 2s
243400K .......... .......... .......... .......... .......... 91% 11.0M 2s
243450K .......... .......... .......... .......... .......... 91% 11.1M 2s
243500K .......... .......... .......... .......... .......... 91% 14.8M 2s
243550K .......... .......... .......... .......... .......... 91% 16.9M 2s
243600K .......... .......... .......... .......... .......... 91% 12.9M 2s
243650K .......... .......... .......... .......... .......... 91% 13.8M 2s
243700K .......... .......... .......... .......... .......... 91% 7.88M 2s
243750K .......... .......... .......... .......... .......... 91% 7.03M 2s
243800K .......... .......... .......... .......... .......... 91% 7.26M 2s
243850K .......... .......... .......... .......... .......... 91% 11.9M 2s
243900K .......... .......... .......... .......... .......... 91% 13.9M 2s
243950K .......... .......... .......... .......... .......... 91% 14.0M 2s
244000K .......... .......... .......... .......... .......... 91% 15.6M 2s
244050K .......... .......... .......... .......... .......... 91% 18.6M 2s
244100K .......... .......... .......... .......... .......... 91% 17.2M 2s
244150K .......... .......... .......... .......... .......... 91% 16.6M 2s
244200K .......... .......... .......... .......... .......... 91% 16.2M 2s
244250K .......... .......... .......... .......... .......... 91% 13.4M 2s
244300K .......... .......... .......... .......... .......... 91% 13.5M 2s
244350K .......... .......... .......... .......... .......... 91% 9.49M 2s
244400K .......... .......... .......... .......... .......... 91% 9.86M 2s
244450K .......... .......... .......... .......... .......... 91% 6.61M 2s
244500K .......... .......... .......... .......... .......... 92% 9.49M 2s
244550K .......... .......... .......... .......... .......... 92% 8.05M 2s
244600K .......... .......... .......... .......... .......... 92% 12.8M 2s
244650K .......... .......... .......... .......... .......... 92% 15.3M 2s
244700K .......... .......... .......... .......... .......... 92% 10.3M 2s
244750K .......... .......... .......... .......... .......... 92% 18.3M 2s
244800K .......... .......... .......... .......... .......... 92% 10.9M 2s
244850K .......... .......... .......... .......... .......... 92% 8.85M 2s
244900K .......... .......... .......... .......... .......... 92% 8.40M 2s
244950K .......... .......... .......... .......... .......... 92% 6.66M 2s
245000K .......... .......... .......... .......... .......... 92% 6.48M 2s
245050K .......... .......... .......... .......... .......... 92% 5.45M 2s
245100K .......... .......... .......... .......... .......... 92% 15.6M 2s
245150K .......... .......... .......... .......... .......... 92% 14.0M 2s
245200K .......... .......... .......... .......... .......... 92% 15.5M 2s
245250K .......... .......... .......... .......... .......... 92% 15.3M 2s
245300K .......... .......... .......... .......... .......... 92% 20.0M 2s
245350K .......... .......... .......... .......... .......... 92% 15.8M 2s
245400K .......... .......... .......... .......... .......... 92% 15.0M 2s
245450K .......... .......... .......... .......... .......... 92% 16.0M 2s
245500K .......... .......... .......... .......... .......... 92% 17.3M 2s
245550K .......... .......... .......... .......... .......... 92% 19.9M 2s
245600K .......... .......... .......... .......... .......... 92% 14.8M 2s
245650K .......... .......... .......... .......... .......... 92% 23.4M 2s
245700K .......... .......... .......... .......... .......... 92% 14.0M 2s
245750K .......... .......... .......... .......... .......... 92% 13.4M 2s
245800K .......... .......... .......... .......... .......... 92% 16.9M 2s
245850K .......... .......... .......... .......... .......... 92% 14.8M 2s
245900K .......... .......... .......... .......... .......... 92% 11.4M 2s
245950K .......... .......... .......... .......... .......... 92% 13.9M 2s
246000K .......... .......... .......... .......... .......... 92% 9.62M 2s
246050K .......... .......... .......... .......... .......... 92% 10.7M 2s
246100K .......... .......... .......... .......... .......... 92% 8.91M 2s
246150K .......... .......... .......... .......... .......... 92% 8.84M 2s
246200K .......... .......... .......... .......... .......... 92% 12.1M 2s
246250K .......... .......... .......... .......... .......... 92% 16.1M 2s
246300K .......... .......... .......... .......... .......... 92% 12.2M 2s
246350K .......... .......... .......... .......... .......... 92% 8.32M 2s
246400K .......... .......... .......... .......... .......... 92% 8.55M 2s
246450K .......... .......... .......... .......... .......... 92% 4.59M 2s
246500K .......... .......... .......... .......... .......... 92% 5.83M 2s
246550K .......... .......... .......... .......... .......... 92% 7.06M 2s
246600K .......... .......... .......... .......... .......... 92% 4.80M 2s
246650K .......... .......... .......... .......... .......... 92% 6.12M 2s
246700K .......... .......... .......... .......... .......... 92% 6.93M 2s
246750K .......... .......... .......... .......... .......... 92% 4.23M 2s
246800K .......... .......... .......... .......... .......... 92% 3.93M 2s
246850K .......... .......... .......... .......... .......... 92% 1.81M 2s
246900K .......... .......... .......... .......... .......... 92% 3.84M 2s
246950K .......... .......... .......... .......... .......... 92% 2.91M 2s
247000K .......... .......... .......... .......... .......... 92% 4.28M 2s
247050K .......... .......... .......... .......... .......... 92% 1.76M 2s
247100K .......... .......... .......... .......... .......... 92% 1.58M 2s
247150K .......... .......... .......... .......... .......... 93% 5.58M 2s
247200K .......... .......... .......... .......... .......... 93% 4.11M 2s
247250K .......... .......... .......... .......... .......... 93% 4.57M 2s
247300K .......... .......... .......... .......... .......... 93% 4.84M 2s
247350K .......... .......... .......... .......... .......... 93% 3.59M 2s
247400K .......... .......... .......... .......... .......... 93% 6.14M 2s
247450K .......... .......... .......... .......... .......... 93% 16.8M 2s
247500K .......... .......... .......... .......... .......... 93% 33.2M 2s
247550K .......... .......... .......... .......... .......... 93% 34.5M 2s
247600K .......... .......... .......... .......... .......... 93% 25.6M 2s
247650K .......... .......... .......... .......... .......... 93% 20.0M 2s
247700K .......... .......... .......... .......... .......... 93% 25.9M 2s
247750K .......... .......... .......... .......... .......... 93% 33.0M 2s
247800K .......... .......... .......... .......... .......... 93% 14.7M 2s
247850K .......... .......... .......... .......... .......... 93% 18.4M 2s
247900K .......... .......... .......... .......... .......... 93% 24.2M 2s
247950K .......... .......... .......... .......... .......... 93% 16.7M 2s
248000K .......... .......... .......... .......... .......... 93% 16.1M 2s
248050K .......... .......... .......... .......... .......... 93% 16.5M 2s
248100K .......... .......... .......... .......... .......... 93% 20.8M 2s
248150K .......... .......... .......... .......... .......... 93% 20.3M 2s
248200K .......... .......... .......... .......... .......... 93% 17.6M 2s
248250K .......... .......... .......... .......... .......... 93% 20.3M 2s
248300K .......... .......... .......... .......... .......... 93% 23.3M 2s
248350K .......... .......... .......... .......... .......... 93% 12.6M 2s
248400K .......... .......... .......... .......... .......... 93% 19.6M 2s
248450K .......... .......... .......... .......... .......... 93% 17.6M 2s
248500K .......... .......... .......... .......... .......... 93% 14.2M 2s
248550K .......... .......... .......... .......... .......... 93% 16.7M 2s
248600K .......... .......... .......... .......... .......... 93% 14.3M 2s
248650K .......... .......... .......... .......... .......... 93% 14.2M 2s
248700K .......... .......... .......... .......... .......... 93% 14.3M 2s
248750K .......... .......... .......... .......... .......... 93% 12.2M 2s
248800K .......... .......... .......... .......... .......... 93% 12.6M 2s
248850K .......... .......... .......... .......... .......... 93% 10.4M 2s
248900K .......... .......... .......... .......... .......... 93% 11.5M 2s
248950K .......... .......... .......... .......... .......... 93% 6.90M 2s
249000K .......... .......... .......... .......... .......... 93% 12.2M 2s
249050K .......... .......... .......... .......... .......... 93% 9.44M 2s
249100K .......... .......... .......... .......... .......... 93% 18.5M 2s
249150K .......... .......... .......... .......... .......... 93% 18.0M 2s
249200K .......... .......... .......... .......... .......... 93% 17.1M 2s
249250K .......... .......... .......... .......... .......... 93% 26.3M 2s
249300K .......... .......... .......... .......... .......... 93% 15.4M 2s
249350K .......... .......... .......... .......... .......... 93% 16.8M 2s
249400K .......... .......... .......... .......... .......... 93% 23.3M 2s
249450K .......... .......... .......... .......... .......... 93% 13.8M 2s
249500K .......... .......... .......... .......... .......... 93% 22.5M 2s
249550K .......... .......... .......... .......... .......... 93% 22.2M 2s
249600K .......... .......... .......... .......... .......... 93% 15.9M 2s
249650K .......... .......... .......... .......... .......... 93% 12.4M 2s
249700K .......... .......... .......... .......... .......... 93% 9.60M 2s
249750K .......... .......... .......... .......... .......... 93% 12.3M 2s
249800K .......... .......... .......... .......... .......... 94% 14.2M 2s
249850K .......... .......... .......... .......... .......... 94% 18.2M 2s
249900K .......... .......... .......... .......... .......... 94% 17.3M 2s
249950K .......... .......... .......... .......... .......... 94% 16.0M 2s
250000K .......... .......... .......... .......... .......... 94% 15.5M 2s
250050K .......... .......... .......... .......... .......... 94% 19.4M 2s
250100K .......... .......... .......... .......... .......... 94% 14.9M 2s
250150K .......... .......... .......... .......... .......... 94% 16.9M 2s
250200K .......... .......... .......... .......... .......... 94% 12.3M 2s
250250K .......... .......... .......... .......... .......... 94% 14.5M 2s
250300K .......... .......... .......... .......... .......... 94% 14.5M 2s
250350K .......... .......... .......... .......... .......... 94% 14.8M 2s
250400K .......... .......... .......... .......... .......... 94% 15.8M 1s
250450K .......... .......... .......... .......... .......... 94% 14.6M 1s
250500K .......... .......... .......... .......... .......... 94% 15.6M 1s
250550K .......... .......... .......... .......... .......... 94% 17.0M 1s
250600K .......... .......... .......... .......... .......... 94% 11.1M 1s
250650K .......... .......... .......... .......... .......... 94% 14.5M 1s
250700K .......... .......... .......... .......... .......... 94% 10.9M 1s
250750K .......... .......... .......... .......... .......... 94% 18.7M 1s
250800K .......... .......... .......... .......... .......... 94% 19.8M 1s
250850K .......... .......... .......... .......... .......... 94% 16.3M 1s
250900K .......... .......... .......... .......... .......... 94% 16.1M 1s
250950K .......... .......... .......... .......... .......... 94% 14.8M 1s
251000K .......... .......... .......... .......... .......... 94% 11.7M 1s
251050K .......... .......... .......... .......... .......... 94% 19.4M 1s
251100K .......... .......... .......... .......... .......... 94% 15.6M 1s
251150K .......... .......... .......... .......... .......... 94% 18.2M 1s
251200K .......... .......... .......... .......... .......... 94% 14.9M 1s
251250K .......... .......... .......... .......... .......... 94% 20.1M 1s
251300K .......... .......... .......... .......... .......... 94% 14.7M 1s
251350K .......... .......... .......... .......... .......... 94% 9.78M 1s
251400K .......... .......... .......... .......... .......... 94% 13.6M 1s
251450K .......... .......... .......... .......... .......... 94% 13.0M 1s
251500K .......... .......... .......... .......... .......... 94% 20.9M 1s
251550K .......... .......... .......... .......... .......... 94% 11.9M 1s
251600K .......... .......... .......... .......... .......... 94% 38.6M 1s
251650K .......... .......... .......... .......... .......... 94% 17.3M 1s
251700K .......... .......... .......... .......... .......... 94% 17.2M 1s
251750K .......... .......... .......... .......... .......... 94% 14.3M 1s
251800K .......... .......... .......... .......... .......... 94% 19.0M 1s
251850K .......... .......... .......... .......... .......... 94% 24.5M 1s
251900K .......... .......... .......... .......... .......... 94% 24.1M 1s
251950K .......... .......... .......... .......... .......... 94% 22.9M 1s
252000K .......... .......... .......... .......... .......... 94% 20.8M 1s
252050K .......... .......... .......... .......... .......... 94% 27.3M 1s
252100K .......... .......... .......... .......... .......... 94% 18.8M 1s
252150K .......... .......... .......... .......... .......... 94% 29.3M 1s
252200K .......... .......... .......... .......... .......... 94% 22.8M 1s
252250K .......... .......... .......... .......... .......... 94% 19.0M 1s
252300K .......... .......... .......... .......... .......... 94% 18.0M 1s
252350K .......... .......... .......... .......... .......... 94% 24.1M 1s
252400K .......... .......... .......... .......... .......... 94% 28.8M 1s
252450K .......... .......... .......... .......... .......... 95% 26.3M 1s
252500K .......... .......... .......... .......... .......... 95% 28.9M 1s
252550K .......... .......... .......... .......... .......... 95% 31.0M 1s
252600K .......... .......... .......... .......... .......... 95% 21.5M 1s
252650K .......... .......... .......... .......... .......... 95% 24.4M 1s
252700K .......... .......... .......... .......... .......... 95% 19.5M 1s
252750K .......... .......... .......... .......... .......... 95% 21.4M 1s
252800K .......... .......... .......... .......... .......... 95% 21.2M 1s
252850K .......... .......... .......... .......... .......... 95% 18.6M 1s
252900K .......... .......... .......... .......... .......... 95% 19.1M 1s
252950K .......... .......... .......... .......... .......... 95% 25.3M 1s
253000K .......... .......... .......... .......... .......... 95% 32.6M 1s
253050K .......... .......... .......... .......... .......... 95% 26.2M 1s
253100K .......... .......... .......... .......... .......... 95% 18.9M 1s
253150K .......... .......... .......... .......... .......... 95% 24.0M 1s
253200K .......... .......... .......... .......... .......... 95% 17.2M 1s
253250K .......... .......... .......... .......... .......... 95% 20.7M 1s
253300K .......... .......... .......... .......... .......... 95% 27.0M 1s
253350K .......... .......... .......... .......... .......... 95% 29.2M 1s
253400K .......... .......... .......... .......... .......... 95% 21.3M 1s
253450K .......... .......... .......... .......... .......... 95% 23.5M 1s
253500K .......... .......... .......... .......... .......... 95% 35.0M 1s
253550K .......... .......... .......... .......... .......... 95% 21.2M 1s
253600K .......... .......... .......... .......... .......... 95% 22.0M 1s
253650K .......... .......... .......... .......... .......... 95% 21.9M 1s
253700K .......... .......... .......... .......... .......... 95% 10.1M 1s
253750K .......... .......... .......... .......... .......... 95% 12.8M 1s
253800K .......... .......... .......... .......... .......... 95% 12.2M 1s
253850K .......... .......... .......... .......... .......... 95% 12.6M 1s
253900K .......... .......... .......... .......... .......... 95% 13.0M 1s
253950K .......... .......... .......... .......... .......... 95% 8.21M 1s
254000K .......... .......... .......... .......... .......... 95% 10.7M 1s
254050K .......... .......... .......... .......... .......... 95% 6.72M 1s
254100K .......... .......... .......... .......... .......... 95% 4.16M 1s
254150K .......... .......... .......... .......... .......... 95% 5.51M 1s
254200K .......... .......... .......... .......... .......... 95% 7.10M 1s
254250K .......... .......... .......... .......... .......... 95% 17.7M 1s
254300K .......... .......... .......... .......... .......... 95% 32.1M 1s
254350K .......... .......... .......... .......... .......... 95% 39.2M 1s
254400K .......... .......... .......... .......... .......... 95% 42.4M 1s
254450K .......... .......... .......... .......... .......... 95% 33.5M 1s
254500K .......... .......... .......... .......... .......... 95% 41.0M 1s
254550K .......... .......... .......... .......... .......... 95% 25.1M 1s
254600K .......... .......... .......... .......... .......... 95% 48.0M 1s
254650K .......... .......... .......... .......... .......... 95% 46.9M 1s
254700K .......... .......... .......... .......... .......... 95% 35.4M 1s
254750K .......... .......... .......... .......... .......... 95% 27.8M 1s
254800K .......... .......... .......... .......... .......... 95% 19.9M 1s
254850K .......... .......... .......... .......... .......... 95% 56.2M 1s
254900K .......... .......... .......... .......... .......... 95% 33.0M 1s
254950K .......... .......... .......... .......... .......... 95% 17.6M 1s
255000K .......... .......... .......... .......... .......... 95% 24.5M 1s
255050K .......... .......... .......... .......... .......... 95% 18.8M 1s
255100K .......... .......... .......... .......... .......... 96% 11.6M 1s
255150K .......... .......... .......... .......... .......... 96% 13.9M 1s
255200K .......... .......... .......... .......... .......... 96% 10.7M 1s
255250K .......... .......... .......... .......... .......... 96% 11.2M 1s
255300K .......... .......... .......... .......... .......... 96% 14.5M 1s
255350K .......... .......... .......... .......... .......... 96% 17.6M 1s
255400K .......... .......... .......... .......... .......... 96% 28.7M 1s
255450K .......... .......... .......... .......... .......... 96% 18.8M 1s
255500K .......... .......... .......... .......... .......... 96% 24.7M 1s
255550K .......... .......... .......... .......... .......... 96% 20.5M 1s
255600K .......... .......... .......... .......... .......... 96% 19.8M 1s
255650K .......... .......... .......... .......... .......... 96% 23.9M 1s
255700K .......... .......... .......... .......... .......... 96% 16.9M 1s
255750K .......... .......... .......... .......... .......... 96% 25.1M 1s
255800K .......... .......... .......... .......... .......... 96% 23.6M 1s
255850K .......... .......... .......... .......... .......... 96% 15.8M 1s
255900K .......... .......... .......... .......... .......... 96% 23.0M 1s
255950K .......... .......... .......... .......... .......... 96% 19.6M 1s
256000K .......... .......... .......... .......... .......... 96% 29.3M 1s
256050K .......... .......... .......... .......... .......... 96% 17.6M 1s
256100K .......... .......... .......... .......... .......... 96% 17.2M 1s
256150K .......... .......... .......... .......... .......... 96% 21.7M 1s
256200K .......... .......... .......... .......... .......... 96% 15.7M 1s
256250K .......... .......... .......... .......... .......... 96% 17.5M 1s
256300K .......... .......... .......... .......... .......... 96% 15.4M 1s
256350K .......... .......... .......... .......... .......... 96% 10.4M 1s
256400K .......... .......... .......... .......... .......... 96% 8.01M 1s
256450K .......... .......... .......... .......... .......... 96% 7.95M 1s
256500K .......... .......... .......... .......... .......... 96% 7.73M 1s
256550K .......... .......... .......... .......... .......... 96% 9.33M 1s
256600K .......... .......... .......... .......... .......... 96% 7.46M 1s
256650K .......... .......... .......... .......... .......... 96% 8.07M 1s
256700K .......... .......... .......... .......... .......... 96% 7.68M 1s
256750K .......... .......... .......... .......... .......... 96% 14.5M 1s
256800K .......... .......... .......... .......... .......... 96% 11.4M 1s
256850K .......... .......... .......... .......... .......... 96% 10.2M 1s
256900K .......... .......... .......... .......... .......... 96% 9.59M 1s
256950K .......... .......... .......... .......... .......... 96% 7.72M 1s
257000K .......... .......... .......... .......... .......... 96% 12.2M 1s
257050K .......... .......... .......... .......... .......... 96% 14.6M 1s
257100K .......... .......... .......... .......... .......... 96% 23.8M 1s
257150K .......... .......... .......... .......... .......... 96% 24.6M 1s
257200K .......... .......... .......... .......... .......... 96% 18.6M 1s
257250K .......... .......... .......... .......... .......... 96% 21.7M 1s
257300K .......... .......... .......... .......... .......... 96% 25.5M 1s
257350K .......... .......... .......... .......... .......... 96% 17.9M 1s
257400K .......... .......... .......... .......... .......... 96% 18.8M 1s
257450K .......... .......... .......... .......... .......... 96% 26.0M 1s
257500K .......... .......... .......... .......... .......... 96% 12.4M 1s
257550K .......... .......... .......... .......... .......... 96% 13.2M 1s
257600K .......... .......... .......... .......... .......... 96% 14.6M 1s
257650K .......... .......... .......... .......... .......... 96% 20.5M 1s
257700K .......... .......... .......... .......... .......... 96% 21.6M 1s
257750K .......... .......... .......... .......... .......... 96% 22.0M 1s
257800K .......... .......... .......... .......... .......... 97% 25.4M 1s
257850K .......... .......... .......... .......... .......... 97% 16.6M 1s
257900K .......... .......... .......... .......... .......... 97% 24.0M 1s
257950K .......... .......... .......... .......... .......... 97% 14.9M 1s
258000K .......... .......... .......... .......... .......... 97% 17.9M 1s
258050K .......... .......... .......... .......... .......... 97% 10.6M 1s
258100K .......... .......... .......... .......... .......... 97% 11.2M 1s
258150K .......... .......... .......... .......... .......... 97% 10.1M 1s
258200K .......... .......... .......... .......... .......... 97% 16.4M 1s
258250K .......... .......... .......... .......... .......... 97% 16.5M 1s
258300K .......... .......... .......... .......... .......... 97% 14.0M 1s
258350K .......... .......... .......... .......... .......... 97% 12.6M 1s
258400K .......... .......... .......... .......... .......... 97% 15.5M 1s
258450K .......... .......... .......... .......... .......... 97% 12.8M 1s
258500K .......... .......... .......... .......... .......... 97% 20.3M 1s
258550K .......... .......... .......... .......... .......... 97% 23.2M 1s
258600K .......... .......... .......... .......... .......... 97% 18.3M 1s
258650K .......... .......... .......... .......... .......... 97% 25.5M 1s
258700K .......... .......... .......... .......... .......... 97% 12.4M 1s
258750K .......... .......... .......... .......... .......... 97% 25.5M 1s
258800K .......... .......... .......... .......... .......... 97% 16.2M 1s
258850K .......... .......... .......... .......... .......... 97% 14.3M 1s
258900K .......... .......... .......... .......... .......... 97% 22.7M 1s
258950K .......... .......... .......... .......... .......... 97% 16.0M 1s
259000K .......... .......... .......... .......... .......... 97% 23.0M 1s
259050K .......... .......... .......... .......... .......... 97% 20.5M 1s
259100K .......... .......... .......... .......... .......... 97% 20.8M 1s
259150K .......... .......... .......... .......... .......... 97% 24.1M 1s
259200K .......... .......... .......... .......... .......... 97% 17.0M 1s
259250K .......... .......... .......... .......... .......... 97% 23.2M 1s
259300K .......... .......... .......... .......... .......... 97% 20.8M 1s
259350K .......... .......... .......... .......... .......... 97% 17.8M 1s
259400K .......... .......... .......... .......... .......... 97% 19.7M 1s
259450K .......... .......... .......... .......... .......... 97% 19.9M 1s
259500K .......... .......... .......... .......... .......... 97% 22.1M 1s
259550K .......... .......... .......... .......... .......... 97% 16.8M 1s
259600K .......... .......... .......... .......... .......... 97% 13.1M 1s
259650K .......... .......... .......... .......... .......... 97% 18.4M 1s
259700K .......... .......... .......... .......... .......... 97% 11.7M 1s
259750K .......... .......... .......... .......... .......... 97% 11.7M 1s
259800K .......... .......... .......... .......... .......... 97% 11.6M 1s
259850K .......... .......... .......... .......... .......... 97% 18.0M 1s
259900K .......... .......... .......... .......... .......... 97% 55.0M 1s
259950K .......... .......... .......... .......... .......... 97% 18.5M 1s
260000K .......... .......... .......... .......... .......... 97% 41.6M 1s
260050K .......... .......... .......... .......... .......... 97% 28.2M 1s
260100K .......... .......... .......... .......... .......... 97% 24.8M 1s
260150K .......... .......... .......... .......... .......... 97% 29.5M 1s
260200K .......... .......... .......... .......... .......... 97% 22.2M 1s
260250K .......... .......... .......... .......... .......... 97% 24.6M 1s
260300K .......... .......... .......... .......... .......... 97% 28.2M 1s
260350K .......... .......... .......... .......... .......... 97% 20.0M 1s
260400K .......... .......... .......... .......... .......... 97% 25.7M 1s
260450K .......... .......... .......... .......... .......... 98% 25.5M 1s
260500K .......... .......... .......... .......... .......... 98% 24.4M 1s
260550K .......... .......... .......... .......... .......... 98% 26.7M 0s
260600K .......... .......... .......... .......... .......... 98% 18.0M 0s
260650K .......... .......... .......... .......... .......... 98% 14.2M 0s
260700K .......... .......... .......... .......... .......... 98% 24.2M 0s
260750K .......... .......... .......... .......... .......... 98% 18.4M 0s
260800K .......... .......... .......... .......... .......... 98% 21.6M 0s
260850K .......... .......... .......... .......... .......... 98% 24.2M 0s
260900K .......... .......... .......... .......... .......... 98% 13.1M 0s
260950K .......... .......... .......... .......... .......... 98% 14.0M 0s
261000K .......... .......... .......... .......... .......... 98% 18.2M 0s
261050K .......... .......... .......... .......... .......... 98% 13.1M 0s
261100K .......... .......... .......... .......... .......... 98% 11.2M 0s
261150K .......... .......... .......... .......... .......... 98% 13.3M 0s
261200K .......... .......... .......... .......... .......... 98% 12.8M 0s
261250K .......... .......... .......... .......... .......... 98% 15.2M 0s
261300K .......... .......... .......... .......... .......... 98% 15.8M 0s
261350K .......... .......... .......... .......... .......... 98% 13.8M 0s
261400K .......... .......... .......... .......... .......... 98% 37.9M 0s
261450K .......... .......... .......... .......... .......... 98% 37.3M 0s
261500K .......... .......... .......... .......... .......... 98% 63.3M 0s
261550K .......... .......... .......... .......... .......... 98% 75.1M 0s
261600K .......... .......... .......... .......... .......... 98% 21.5M 0s
261650K .......... .......... .......... .......... .......... 98% 129M 0s
261700K .......... .......... .......... .......... .......... 98% 61.5M 0s
261750K .......... .......... .......... .......... .......... 98% 57.9M 0s
261800K .......... .......... .......... .......... .......... 98% 56.7M 0s
261850K .......... .......... .......... .......... .......... 98% 48.5M 0s
261900K .......... .......... .......... .......... .......... 98% 44.8M 0s
261950K .......... .......... .......... .......... .......... 98% 19.6M 0s
262000K .......... .......... .......... .......... .......... 98% 160M 0s
262050K .......... .......... .......... .......... .......... 98% 56.9M 0s
262100K .......... .......... .......... .......... .......... 98% 36.5M 0s
262150K .......... .......... .......... .......... .......... 98% 46.8M 0s
262200K .......... .......... .......... .......... .......... 98% 42.8M 0s
262250K .......... .......... .......... .......... .......... 98% 39.7M 0s
262300K .......... .......... .......... .......... .......... 98% 45.4M 0s
262350K .......... .......... .......... .......... .......... 98% 33.4M 0s
262400K .......... .......... .......... .......... .......... 98% 51.0M 0s
262450K .......... .......... .......... .......... .......... 98% 37.8M 0s
262500K .......... .......... .......... .......... .......... 98% 41.4M 0s
262550K .......... .......... .......... .......... .......... 98% 30.8M 0s
262600K .......... .......... .......... .......... .......... 98% 21.4M 0s
262650K .......... .......... .......... .......... .......... 98% 76.5M 0s
262700K .......... .......... .......... .......... .......... 98% 29.9M 0s
262750K .......... .......... .......... .......... .......... 98% 24.3M 0s
262800K .......... .......... .......... .......... .......... 98% 35.4M 0s
262850K .......... .......... .......... .......... .......... 98% 27.9M 0s
262900K .......... .......... .......... .......... .......... 98% 27.9M 0s
262950K .......... .......... .......... .......... .......... 98% 20.8M 0s
263000K .......... .......... .......... .......... .......... 98% 31.9M 0s
263050K .......... .......... .......... .......... .......... 98% 24.3M 0s
263100K .......... .......... .......... .......... .......... 99% 22.1M 0s
263150K .......... .......... .......... .......... .......... 99% 26.2M 0s
263200K .......... .......... .......... .......... .......... 99% 19.9M 0s
263250K .......... .......... .......... .......... .......... 99% 30.3M 0s
263300K .......... .......... .......... .......... .......... 99% 24.0M 0s
263350K .......... .......... .......... .......... .......... 99% 25.4M 0s
263400K .......... .......... .......... .......... .......... 99% 27.1M 0s
263450K .......... .......... .......... .......... .......... 99% 24.1M 0s
263500K .......... .......... .......... .......... .......... 99% 26.4M 0s
263550K .......... .......... .......... .......... .......... 99% 26.5M 0s
263600K .......... .......... .......... .......... .......... 99% 26.0M 0s
263650K .......... .......... .......... .......... .......... 99% 40.9M 0s
263700K .......... .......... .......... .......... .......... 99% 33.8M 0s
263750K .......... .......... .......... .......... .......... 99% 38.9M 0s
263800K .......... .......... .......... .......... .......... 99% 40.4M 0s
263850K .......... .......... .......... .......... .......... 99% 23.5M 0s
263900K .......... .......... .......... .......... .......... 99% 37.2M 0s
263950K .......... .......... .......... .......... .......... 99% 17.9M 0s
264000K .......... .......... .......... .......... .......... 99% 15.1M 0s
264050K .......... .......... .......... .......... .......... 99% 29.3M 0s
264100K .......... .......... .......... .......... .......... 99% 15.7M 0s
264150K .......... .......... .......... .......... .......... 99% 27.1M 0s
264200K .......... .......... .......... .......... .......... 99% 16.2M 0s
264250K .......... .......... .......... .......... .......... 99% 14.9M 0s
264300K .......... .......... .......... .......... .......... 99% 13.8M 0s
264350K .......... .......... .......... .......... .......... 99% 11.6M 0s
264400K .......... .......... .......... .......... .......... 99% 15.6M 0s
264450K .......... .......... .......... .......... .......... 99% 9.56M 0s
264500K .......... .......... .......... .......... .......... 99% 10.9M 0s
264550K .......... .......... .......... .......... .......... 99% 19.2M 0s
264600K .......... .......... .......... .......... .......... 99% 13.1M 0s
264650K .......... .......... .......... .......... .......... 99% 26.3M 0s
264700K .......... .......... .......... .......... .......... 99% 13.9M 0s
264750K .......... .......... .......... .......... .......... 99% 19.7M 0s
264800K .......... .......... .......... .......... .......... 99% 21.9M 0s
264850K .......... .......... .......... .......... .......... 99% 20.2M 0s
264900K .......... .......... .......... .......... .......... 99% 29.0M 0s
264950K .......... .......... .......... .......... .......... 99% 23.1M 0s
265000K .......... .......... .......... .......... .......... 99% 16.8M 0s
265050K .......... .......... .......... .......... .......... 99% 22.6M 0s
265100K .......... .......... .......... .......... .......... 99% 19.1M 0s
265150K .......... .......... .......... .......... .......... 99% 16.3M 0s
265200K .......... .......... .......... .......... .......... 99% 21.5M 0s
265250K .......... .......... .......... .......... .......... 99% 18.8M 0s
265300K .......... .......... .......... .......... .......... 99% 17.6M 0s
265350K .......... .......... .......... .......... .......... 99% 15.8M 0s
265400K .......... .......... .......... .......... .......... 99% 21.8M 0s
265450K .......... .......... .......... .......... .......... 99% 14.6M 0s
265500K .......... .......... .......... .......... .......... 99% 23.6M 0s
265550K .......... .......... .......... .......... .......... 99% 21.9M 0s
265600K .......... .......... .......... .......... .......... 99% 19.6M 0s
265650K .......... .......... .......... .......... .......... 99% 16.8M 0s
265700K .......... .......... .......... .......... .......... 99% 17.6M 0s
265750K .......... .......... .......... 100% 15.6M=25s
2024-06-18 21:17:23 (10.3 MB/s) - ‘ESPbeta.tgz’ saved [272159479/272159479]
+ tar -xf ESPbeta.tgz
+ rm -rf EngSketchPad/data/Slugs
+ python --version
Python 3.11.9
+ [[ '' == *\.\i\f\o\r\t ]]
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/config/
+ ./makeEnv
ESP runtime AutoConfigurator
CASROOT = /home/jenkins/util/ESP/OpenCASCADE-7.8.0 with contents:
bin
include
lib
share
Info: Python exec /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python found!
Info: Python header /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11/Python.h found!
Info: Python library /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/libpython3.11.so found!
ESP_ARCH = LINUX64
ESP_ROOT = /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad
EFCOMP = gfortran
CARCH = LINUX64
CASROOT = /home/jenkins/util/ESP/OpenCASCADE-7.8.0
CASARCH = .
CASREV = 7.8
PYTHONINC= /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11
PYTHONLIB= -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
+ source /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=LINUX64
++ ESP_ARCH=LINUX64
++ export ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad
++ ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad
++ export CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export CASARCH=.
++ CASARCH=.
++ export CASREV=7.8
++ CASREV=7.8
++ export PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONINC=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11
++ PYTHONINC=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11
++ export 'PYTHONLIB=-L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11'
++ PYTHONLIB='-L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11'
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ export AFLR_ARCH=Linux-x86-64
++ AFLR_ARCH=Linux-x86-64
++ '[' -z /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib: ']'
++ export LD_LIBRARY_PATH=/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ LD_LIBRARY_PATH=/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ export CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ export TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ export 'SLUGS_START=firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/SLUGS/Slugs.html &'
++ SLUGS_START='firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/SLUGS/Slugs.html &'
++ export 'ESP_START=firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/ESP/ESP.html &'
++ ESP_START='firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/ESP/ESP.html &'
++ export 'WV_START=firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/wvClient/wv.html &'
++ WV_START='firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/wvClient/wv.html &'
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src
+ make
(cd EGADS/src; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/src'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/LINUX64
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/LINUX64
cp -p ../include/LINUX64 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/LINUX64
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/STANALYZER.make
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/STANALYZER.make
cp -p ../include/STANALYZER.make /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/STANALYZER.make
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.h
cp -p ../include/egads.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads_dot.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads_dot.h
cp -p ../include/egads_dot.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads_dot.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.inc
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.inc
cp -p ../include/egads.inc /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.inc
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsErrors.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsErrors.h
cp -p ../include/egadsErrors.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsErrors.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTypes.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTypes.h
cp -p ../include/egadsTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTypes.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/emp.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/emp.h
cp -p ../include/emp.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/emp.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/prm.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/prm.h
cp -p ../include/prm.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/prm.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.h
cp -p ../include/wsserver.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.inc
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.inc
cp -p ../include/wsserver.inc /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.inc
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsss.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsss.h
cp -p ../include/wsss.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsss.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTris.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTris.h
cp -p egadsTris.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTris.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineFit.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineFit.h
cp -p egadsSplineFit.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineFit.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineVels.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineVels.h
cp -p egadsSplineVels.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineVels.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsf90.inc
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsf90.inc
cp -p ../include/egadsf90.inc /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsf90.inc
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealD.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Lazy.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealD_Lazy.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Trad.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealD_Trad.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealS.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Lazy.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealS_Lazy.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Trad.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealS_Trad.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/always_inline.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/always_inline.h
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsGeom.cpp -o ./egadsGeom.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsHLevel.cpp -o ./egadsHLevel.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsTopo.cpp -o ./egadsTopo.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsCopy.cpp -o ./egadsCopy.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsSpline.cpp -o ./egadsSpline.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsIO.cpp -o ./egadsIO.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsSplineFit.cpp -o ./egadsSplineFit.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsSkinning.cpp -o ./egadsSkinning.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsTessSens.cpp -o ./egadsTessSens.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 OCC/BRepLib_FuseEdges.cpp -o ./BRepLib_FuseEdges.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsBase.c -o ./egadsBase.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsMemory.c -o ./egadsMemory.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsAttrs.c -o ./egadsAttrs.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsTess.c -o ./egadsTess.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsTessInp.c -o ./egadsTessInp.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsTris.c -o ./egadsTris.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsQuads.c -o ./egadsQuads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsFit.c -o ./egadsFit.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsRobust.c -o ./egadsRobust.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsSBO.c -o ./egadsSBO.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap prmCfit.c -o ./prmCfit.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap prmGrid.c -o ./prmGrid.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap prmUV.c -o ./prmUV.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsExport.c -o ./egadsExport.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsEffect.c -o ./egadsEffect.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsSolids.c -o ./egadsSolids.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include ../util/emp.c \
-o ./emp.o
g++ -g -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \
../util/evaluate.c -o ./evaluate.o
g++ -g -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \
../util/rational.c -o ./rational.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include -I../util \
../util/regQuads.c -o ./regQuads.o
g++ -g -o ./SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp
./SurrealD1
SurrealD1_test_suite Complete!
g++ -g -o ./SurrealD4 -O -std=c++11 -I. ../util/SurrealD4_btest.cpp
./SurrealD4
SurrealD4_test_suite Complete!
g++ -g -o ./SurrealS1 -O -std=c++11 -I. ../util/SurrealS1_btest.cpp
./SurrealS1
SurrealS1_test_suite Complete!
g++ -g -o ./SurrealS4 -O -std=c++11 -I. ../util/SurrealS4_btest.cpp
../util/SurrealS4_btest.cpp: In function ‘void multiply_deriv2()’:
../util/SurrealS4_btest.cpp:1265:23: note: variable tracking size limit exceeded with -fvar-tracking-assignments, retrying without
BOOST_AUTO_TEST_CASE( multiply_deriv2 )
^
../util/SurrealS4_btest.cpp:19:42: note: in definition of macro ‘BOOST_AUTO_TEST_CASE’
#define BOOST_AUTO_TEST_CASE( fun ) void fun()
^
./SurrealS4
SurrealS4_test_suite Complete!
make -C ../util
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/util'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 uvmap/main/uvmap.c -Iuvmap \
-o ./uvmap.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_bnd_adj.c -o ./uvmap_bnd_adj.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibfibf.c -o ./uvmap_ibfibf.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_message.c -o ./uvmap_message.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibfin.c -o ./uvmap_ibfin.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_read.c -o ./uvmap_read.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_iccin.c -o ./uvmap_iccin.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_add.c -o ./uvmap_add.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_cpu_message.c -o ./uvmap_cpu_message.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapFindUV.c -o ./EG_uvmapFindUV.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapTest.c -o ./EG_uvmapTest.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_inibe.c -o ./uvmap_inibe.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_version.c -o ./uvmap_version.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_inl_uv_bnd.c -o ./uvmap_inl_uv_bnd.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_chk_edge_ratio.c -o ./uvmap_chk_edge_ratio.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_struct_tasks.c -o ./uvmap_struct_tasks.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmap_Read.c -o ./EG_uvmap_Read.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_idibe.c -o ./uvmap_idibe.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapStructFree.c -o ./EG_uvmapStructFree.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapGen.c -o ./EG_uvmapGen.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_write.c -o ./uvmap_write.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibeibe.c -o ./uvmap_ibeibe.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_chk_area_uv.c -o ./uvmap_chk_area_uv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_norm_uv.c -o ./uvmap_norm_uv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_iccibe.c -o ./uvmap_iccibe.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_malloc.c -o ./uvmap_malloc.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_gen_uv.c -o ./uvmap_gen_uv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_to_egads.c -o ./uvmap_to_egads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmap_Write.c -o ./EG_uvmap_Write.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_test.c -o ./uvmap_test.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_mben_disc.c -o ./uvmap_mben_disc.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_find_uv.c -o ./uvmap_find_uv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_gen.c -o ./uvmap_gen.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_solve.c -o ./uvmap_solve.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_from_egads.c -o ./uvmap_from_egads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 egadsUVmap.c -Iuvmap \
-o ./egadsUVmap.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a ./egadsUVmap.o uvmap_cpu_message.o uvmap_ibfibf.o uvmap_message.o uvmap_version.o uvmap_gen_uv.o uvmap_inl_uv_bnd.o EG_uvmap_Read.o uvmap_chk_edge_ratio.o uvmap_idibe.o uvmap_write.o uvmap_ibeibe.o uvmap_chk_area_uv.o uvmap_gen.o uvmap_malloc.o uvmap_to_egads.o EG_uvmap_Write.o uvmap_iccibe.o EG_uvmapGen.o EG_uvmapTest.o uvmap_read.o uvmap_ibfin.o uvmap_iccin.o uvmap_add.o EG_uvmapFindUV.o uvmap_struct_tasks.o uvmap_bnd_adj.o EG_uvmapStructFree.o uvmap_inibe.o uvmap_norm_uv.o uvmap_test.o uvmap_mben_disc.o uvmap_find_uv.o uvmap_solve.o uvmap_from_egads.o; )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a
gcc -g -o ./uvmap.exe ./uvmap.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -luvmap -lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/util'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegads.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegads.so
(cd .; gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegads.so \
egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o emp.o evaluate.o rational.o regQuads.o \
-L/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -pthread -lm -lstdc++ -lrt )
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadstatic.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadstatic.a
cp /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadstatic.a
(cd .; \
ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadstatic.a egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o emp.o \
evaluate.o rational.o regQuads.o; )
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsBase.c -o ./fgadsBase.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsMemory.c -o ./fgadsMemory.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsAttrs.c -o ./fgadsAttrs.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsTess.c -o ./fgadsTess.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsHLevel.c -o ./fgadsHLevel.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsGeom.c -o ./fgadsGeom.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsTopo.c -o ./fgadsTopo.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libfgads.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libfgads.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libfgads.a fgadsBase.o fgadsMemory.o fgadsAttrs.o fgadsTess.o fgadsHLevel.o fgadsGeom.o fgadsTopo.o; )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libfgads.a
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a emp.o; )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a
*** EGADS Build Complete! ***
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/src'
(cd EGADS/lite; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/lite'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteBase.c -o ./liteBase.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteMemory.c -o ./liteMemory.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteGeom.c -o ./liteGeom.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteTopo.c -o ./liteTopo.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteAttrs.c -o ./liteAttrs.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteImport.c -o ./liteImport.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteString.c -o ./liteString.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../src/egadsTess.c -o ./liteTess.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../src/egadsTris.c -o ./liteTris.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src \
../src/egadsQuads.c -o ./liteQuads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
-I../util ../src/egadsTessInp.c -o ./liteTessInp.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 ../src/egadsRobust.c \
-o ./egadsRobust.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLINUX64 -I../include ../util/emp.c \
-o ./emp.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../util/evaluate.c -o ./evaLite.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE ../util/rational.c \
-o ./ratLite.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I../util \
../util/regQuads.c -o ./liteRegQuads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../src/egadsEffect.c -o ./liteEffect.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
-I../util/uvmap liteUVmap.c -o ./liteUVmap.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslite.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslite.so
(cd .; gcc -g -shared -Wl,-no-undefined \
-o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslite.so liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o liteTess.o liteTris.o \
liteQuads.o liteTessInp.o egadsRobust.o emp.o evaLite.o \
ratLite.o liteRegQuads.o liteEffect.o liteUVmap.o \
-lpthread -lm )
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslitestatic.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslitestatic.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslitestatic.a liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o \
liteTess.o liteTris.o liteQuads.o liteTessInp.o egadsRobust.o \
emp.o evaLite.o ratLite.o liteRegQuads.o liteEffect.o \
liteUVmap.o ; )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslitestatic.a
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/lite'
(cd wvServer; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/wvServer'
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 map.cpp -o ./map.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include base64-decode.c -o ./base64-decode.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include handshake.c -o ./handshake.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include client-handshake.c -o ./client-handshake.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include libwebsockets.c -o ./libwebsockets.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include extension-deflate-stream.c -o ./extension-deflate-stream.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include md5.c -o ./md5.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include extension-x-google-mux.c -o ./extension-x-google-mux.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include parsers.c -o ./parsers.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include extension.c -o ./extension.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include sha-1.c -o ./sha-1.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include server.c -o ./server.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include wv.c -o ./wv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include browserMessage.c -o ./browserMessage.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include fwv.c -o ./fwv.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a map.o base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o \
./fwv.o; )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -DSTANDALONE server.c \
-I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -o ./servertest.o
g++ -g -o ./server ./servertest.o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a \
-lpthread -lz -lm
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.so
(cd .; g++ -g -shared -Wl,-no-undefined \
-o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.so base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o map.o -lz -lpthread)
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/wvServer'
(cd EGADS/examples; make -f egads2cart.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include egads2cart.c \
-o ./egads2cart.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/egads2cart ./egads2cart.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads \
-lrt -lm
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vCurvature.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include vCurvature.c -o ./vCurvature.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vCurvature ./vCurvature.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legads -lrt
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vGeom.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include vGeom.c -o ./vGeom.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vGeom ./vGeom.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legads \
-lrt
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vTess.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include vTess.c -o ./vTess.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include ../util/retessFaces.c \
-o ./retessFaces.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vTesstatic ./vTess.o ./retessFaces.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legadstatic -L/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -pthread -lm \
-lpthread -lz -lrt -lm
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vTess ./vTess.o ./retessFaces.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legads -lrt
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
(cd OpenCSM; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/OpenCSM'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. serveCSM.c -o ./serveCSM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. OpenCSM.c -o ./OpenCSM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udp.c -o ./udp.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. tim.c -o ./tim.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libocsm.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libocsm.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libocsm.so ./OpenCSM.o ./udp.o ./tim.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads -lwsserver -ldl -lrt -lm
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/serveCSM ./serveCSM.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. serveESP.c -o ./serveESP.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/serveESP ./serveESP.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. sensCSM.c -o ./sensCSM.o
gcc -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/sensCSM ./sensCSM.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lrt -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBezier.c -o ./udpBezier.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bezier.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bezier.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bezier.so ./udpBezier.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBiconvex.c -o ./udpBiconvex.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/biconvex.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/biconvex.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/biconvex.so ./udpBiconvex.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBox.c -o ./udpBox.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/box.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/box.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/box.so ./udpBox.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBspline.c -o ./udpBspline.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bspline.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bspline.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bspline.so ./udpBspline.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCatmull.c -o ./udfCatmull.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/catmull.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/catmull.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/catmull.so ./udfCatmull.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCompare.c -o ./udfCompare.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/compare.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/compare.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/compare.so ./udfCompare.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCreateBEM.c -o ./udfCreateBEM.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createBEM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createBEM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createBEM.so ./udfCreateBEM.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCreatePoly.c -o ./udfCreatePoly.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createPoly.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createPoly.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createPoly.so ./udfCreatePoly.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpCsm.c -o ./udpCsm.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/csm.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/csm.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/csm.so ./udpCsm.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfDeform.c -o ./udfDeform.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/deform.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/deform.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/deform.so ./udfDeform.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfDroop.c -o ./udfDroop.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/droop.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/droop.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/droop.so ./udfDroop.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfDumpPmtrs.c -o ./udfDumpPmtrs.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/dumpPmtrs.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/dumpPmtrs.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/dumpPmtrs.so ./udfDumpPmtrs.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfEditAttr.c -o ./udfEditAttr.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/editAttr.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/editAttr.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/editAttr.so ./udfEditAttr.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpEllipse.c -o ./udpEllipse.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ellipse.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ellipse.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ellipse.so ./udpEllipse.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpEqn2body.c -o ./udpEqn2body.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/eqn2body.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/eqn2body.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/eqn2body.so ./udpEqn2body.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpFitcurve.c -o ./udpFitcurve.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fitcurve.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fitcurve.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fitcurve.so ./udpFitcurve.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfFlend.c -o ./udfFlend.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flend.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flend.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flend.so ./udfFlend.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpFreeform.c -o ./udpFreeform.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/freeform.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/freeform.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/freeform.so ./udpFreeform.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfGanged.c -o ./udfGanged.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ganged.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ganged.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ganged.so ./udfGanged.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfGuide.c -o ./udfGuide.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/guide.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/guide.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/guide.so ./udfGuide.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpHex.c -o ./udpHex.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hex.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hex.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hex.so ./udpHex.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpImport.c -o ./udpImport.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/import.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/import.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/import.so ./udpImport.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpKulfan.c -o ./udpKulfan.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/kulfan.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/kulfan.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/kulfan.so ./udpKulfan.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfLinalg.c -o ./udfLinalg.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/linalg.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/linalg.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/linalg.so ./udfLinalg.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfMatchBodys.c -o ./udfMatchBodys.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/matchBodys.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/matchBodys.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/matchBodys.so ./udfMatchBodys.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfMechanism.c -o ./udfMechanism.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mechanism.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mechanism.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mechanism.so ./udfMechanism.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpNaca.c -o ./udpNaca.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca.so ./udpNaca.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfNaca6mc.c -o ./udfNaca6mc.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca6mc.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca6mc.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca6mc.so ./udfNaca6mc.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfNacelle.c -o ./udfNacelle.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nacelle.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nacelle.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nacelle.so ./udfNacelle.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpNurbbody.c -o ./udpNurbbody.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nurbbody.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nurbbody.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nurbbody.so ./udpNurbbody.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfNuscale.c -o ./udfNuscale.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nuscale.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nuscale.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nuscale.so ./udfNuscale.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfOffset.c -o ./udfOffset.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/offset.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/offset.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/offset.so ./udfOffset.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpParabaloid.c -o ./udpParabaloid.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parabaloid.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parabaloid.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parabaloid.so ./udpParabaloid.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpParsec.cpp -o ./udpParsec.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parsec.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parsec.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parsec.so ./udpParsec.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpPod.c -o ./udpPod.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pod.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pod.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pod.so ./udpPod.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpPoly.c -o ./udpPoly.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/poly.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/poly.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/poly.so ./udpPoly.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfPrintBbox.c -o ./udfPrintBbox.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBbox.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBbox.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBbox.so ./udfPrintBbox.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfPrintBrep.c -o ./udfPrintBrep.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBrep.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBrep.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBrep.so ./udfPrintBrep.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfPrintEgo.c -o ./udfPrintEgo.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printEgo.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printEgo.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printEgo.so ./udfPrintEgo.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpProp.c -o ./udpProp.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/prop.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/prop.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/prop.so ./udpProp.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpRadwaf.c -o ./udpRadwaf.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/radwaf.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/radwaf.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/radwaf.so ./udpRadwaf.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpSample.c -o ./udpSample.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sample.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sample.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sample.so ./udpSample.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpSew.c -o ./udpSew.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sew.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sew.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sew.so ./udpSew.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfShadow.c -o ./udfShadow.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/shadow.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/shadow.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/shadow.so ./udfShadow.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfSlices.c -o ./udfSlices.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slices.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slices.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slices.so ./udfSlices.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpStag.c -o ./udpStag.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stag.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stag.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stag.so ./udpStag.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfStiffener.c -o ./udfStiffener.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stiffener.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stiffener.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stiffener.so ./udfStiffener.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpSupell.c -o ./udpSupell.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/supell.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/supell.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/supell.so ./udpSupell.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfTester1.c -o ./udfTester1.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester1.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester1.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester1.so ./udfTester1.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpTester2.c -o ./udpTester2.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester2.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester2.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester2.so ./udpTester2.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpVsp3.c -o ./udpVsp3.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vsp3.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vsp3.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vsp3.so ./udpVsp3.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpWaffle.c -o ./udpWaffle.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/waffle.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/waffle.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/waffle.so ./udpWaffle.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfWarp.c -o ./udfWarp.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/warp.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/warp.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/warp.so ./udfWarp.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. eggPDT2.c -o ./eggPDT2.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/PDT2.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/PDT2.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/PDT2.so ./eggPDT2.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpNaca456.c -o ./udpNaca456.o
gfortran -g -c -O -fPIC -frecursive -fcray-pointer naca456.f90 -o ./naca456.o -J .
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca456.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca456.so
gfortran -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca456.so ./udpNaca456.o ./naca456.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timEreped.c -o ./timEreped.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ereped.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ereped.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ereped.so ./timEreped.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timMitten.c -o ./timMitten.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mitten.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mitten.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mitten.so ./timMitten.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timPlotter.c -o ./timPlotter.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plotter.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plotter.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plotter.so ./timPlotter.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timPlugs.c -o ./timPlugs.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plugs.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plugs.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plugs.so ./timPlugs.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timSlugs.c -o ./timSlugs.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slugs.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slugs.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slugs.so ./timSlugs.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timVspSetup.c -o ./timVspSetup.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vspSetup.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vspSetup.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vspSetup.so ./timVspSetup.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/OpenCSM.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/OpenCSM.h
cp -p OpenCSM.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/OpenCSM.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/common.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/common.h
cp -p common.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/common.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udp.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udp.h
cp -p udp.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udp.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/esp.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/esp.h
cp -p esp.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/esp.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/tim.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/tim.h
cp -p tim.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/tim.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egg.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egg.h
cp -p egg.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egg.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.h
cp -p udpUtilities.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.c
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.c
cp -p udpUtilities.c /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.c
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/OpenCSM'
(cd Slugs; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/Slugs'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. Slugs.c -o ./Slugs.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. Fitter.c \
-o ./Fitter.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. RedBlackTree.c \
-o ./RedBlackTree.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. Tessellate.c \
-o ./Tessellate.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/Slugs ./Slugs.o ./Fitter.o ./RedBlackTree.o \
./Tessellate.o -lrt -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legads \
-lpthread -lz -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. TestFit.c -o ./TestFit.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/TestFit ./TestFit.o ./Fitter.o -lrt -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads \
-lpthread -lz -lm
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/Slugs'
(cd CAPS; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS'
/bin/cp Cart3D/X86_64_GCC/libc3dio.a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libc3dio.a
/bin/cp Cart3D/X86_64_GCC/libCart3D.a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libCart3D.a
/bin/cp Executables/LINUX64/avl /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/avl
/bin/cp Executables/LINUX64/pplot /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/pplot
/bin/cp Executables/LINUX64/pxplot /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/pxplot
/bin/cp Executables/LINUX64/xfoil /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/xfoil
/bin/cp Executables/LINUX64/mastros.exe /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/mastros.exe
/bin/cp Executables/LINUX64/ASTRO.D01 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/ASTRO.D01
/bin/cp Executables/LINUX64/ASTRO.IDX /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/ASTRO.IDX
/bin/cp Executables/LINUX64/mses /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/mses
/bin/cp Executables/LINUX64/mset /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/mset
/bin/cp Libraries/LINUX64/aflr2AIM.so /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/aflr2AIM.so
/bin/cp Libraries/LINUX64/aflr3AIM.so /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/aflr3AIM.so
/bin/cp Libraries/LINUX64/aflr4AIM.so /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/aflr4AIM.so
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS'
(cd CAPS/src; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/src'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/caps.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/caps.h
cp -p ../include/caps.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/caps.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsErrors.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsErrors.h
cp -p ../include/capsErrors.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsErrors.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsTypes.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsTypes.h
cp -p ../include/capsTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsTypes.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimUtil.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimUtil.h
cp -p ../include/aimUtil.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimUtil.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimMesh.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimMesh.h
cp -p ../include/aimMesh.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimMesh.h
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../include \
-I/usr/include/udunits2 aimUtil.c -o ./aimUtil.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include \
-I/usr/include/udunits2 aimTransferUtil.c \
-o ./aimTransferUtil.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../include \
aimMesh.c -o ./aimMesh.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libaimUtil.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libaimUtil.a
ar -rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libaimUtil.a ./aimUtil.o ./aimMesh.o \
./aimTransferUtil.o
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libaimUtil.a
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsBase.c -o ./capsBase.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsAnalysis.c -o ./capsAnalysis.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsApprox.c -o ./capsApprox.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsAttr.c -o ./capsAttr.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsAIM.c -o ./capsAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsBound.c -o ./capsBound.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsProblem.c -o ./capsProblem.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsValue.c -o ./capsValue.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsUnits.c -o ./capsUnits.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 conjGrad.c -o ./conjGrad.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsFunIDs.c -o ./capsFunIDs.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsChkInpt.c -o ./capsChkInpt.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 printObject.c -o ./printObject.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcaps.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcaps.so
(cd .; gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcaps.so \
capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -ludunits2 -locsm -legads -ldl \
-lrt -lm )
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcapsstatic.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcapsstatic.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcapsstatic.a capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcapsstatic.a
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include testingAIM.c \
-o ./testingAIM.o
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so
rm: cannot remove ‘/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so’: No such file or directory
make[1]: [/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so] Error 1 (ignored)
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so ./testingAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include testingWriter.c \
-o ./testingWriter.o
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so
rm: cannot remove ‘/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so’: No such file or directory
make[1]: [/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so] Error 1 (ignored)
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so ./testingWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -ldl -lrt -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include phaseUtil.c \
-o ./phaseUtil.o
gcc -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/phaseUtil ./phaseUtil.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -ludunits2 -locsm -legads -ldl -lrt -lm
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/src'
(cd ../CAPSexamples; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples'
(make -C cCAPS -f aeroelastic_SU2.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o
gcc -g -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include avlTest.c -o ./avlTest.o
gcc -g -o ./avlTest ./avlTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include awaveTest.c -o ./awaveTest.o
gcc -g -o ./awaveTest ./awaveTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include frictionTest.c -o ./frictionTest.o
gcc -g -o ./frictionTest ./frictionTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include fun3dAFLR2Test.c -o ./fun3dAFLR2Test.o
gcc -g -o ./fun3dAFLR2Test ./fun3dAFLR2Test.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include fun3dTetgenTest.c -o ./fun3dTetgenTest.o
gcc -g -o ./fun3dTetgenTest ./fun3dTetgenTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include aeroelasticTest.c -o ./aeroelasticTest.o
gcc -g -o ./aeroelasticTest ./aeroelasticTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f hsm.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmTest.c -o ./hsmTest.o
gcc -g -o ./hsmTest ./hsmTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmSimplePlateTest.c -o ./hsmSimplePlateTest.o
gcc -g -o ./hsmSimplePlateTest ./hsmSimplePlateTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmCantileverPlateTest.c -o ./hsmCantileverPlateTest.o
gcc -g -o ./hsmCantileverPlateTest ./hsmCantileverPlateTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmJoinedPlateTest.c -o ./hsmJoinedPlateTest.o
gcc -g -o ./hsmJoinedPlateTest ./hsmJoinedPlateTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include interferenceTest.c \
-o ./interferenceTest.o
gcc -g -o ./interferenceTest ./interferenceTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include msesTest.c -o ./msesTest.o
gcc -g -o ./msesTest ./msesTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f mystran.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include mystranTest.c -o ./mystranTest.o
gcc -g -o ./mystranTest ./mystranTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include pointwiseTest.c -o ./pointwiseTest.o
gcc -g -o ./pointwiseTest ./pointwiseTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples'
(cd CAPS/aim; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim'
make -C utils
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/utils'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython attrUtils.c -o ./attrUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython meshUtils.c -o ./meshUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cfdUtils.c -o ./cfdUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython miscUtils.c -o ./miscUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython feaUtils.c -o ./feaUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython vlmUtils.c -o ./vlmUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranCards.c -o ./nastranCards.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranUtils.c -o ./nastranUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython tecplotUtils.c -o ./tecplotUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython arrayUtils.c -o ./arrayUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython deprecateUtils.c -o ./deprecateUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cardUtils.c -o ./cardUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython jsonUtils.c -o ./jsonUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cython/nastranOP2Reader.c -o ./nastranOP2Reader.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. vlmSpanSpace.cpp -o ./vlmSpanSpace.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libutils.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libutils.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libutils.a attrUtils.o meshUtils.o cfdUtils.o miscUtils.o feaUtils.o vlmUtils.o nastranCards.o nastranUtils.o tecplotUtils.o arrayUtils.o deprecateUtils.o cardUtils.o jsonUtils.o nastranOP2Reader.o vlmSpanSpace.o )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libutils.a
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils
cp -p -f attrUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/attrUtils.h
cp -p -f nastranCards.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/nastranCards.h
cp -p -f cfdTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cfdTypes.h
cp -p -f arrayUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/arrayUtils.h
cp -p -f meshUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/meshUtils.h
cp -p -f feaTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/feaTypes.h
cp -p -f miscUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/miscUtils.h
cp -p -f meshTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/meshTypes.h
cp -p -f attrTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/attrTypes.h
cp -p -f vlmTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/vlmTypes.h
cp -p -f feaUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/feaUtils.h
cp -p -f cfdUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cfdUtils.h
cp -p -f vlmUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/vlmUtils.h
cp -p -f cardTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cardTypes.h
cp -p -f jsonUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/jsonUtils.h
cp -p -f nastranUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/nastranUtils.h
cp -p -f deprecateUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/deprecateUtils.h
cp -p -f miscTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/miscTypes.h
cp -p -f tecplotUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/tecplotUtils.h
cp -p -f vlmSpanSpace.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/vlmSpanSpace.h
cp -p -f cardUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cardUtils.h
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/utils'
make -C friction
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/friction'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -Wno-format -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils frictionAIM.c \
-o ./frictionAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/frictionAIM.so ./frictionAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
gfortran -g -c -O -fPIC -frecursive -fcray-pointer friction_eja_mod.f -o ./friction.o
gfortran -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/friction ./friction.o
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/friction'
make -C tetgen
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tetgen'
g++ -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils tetgenAIM.cpp \
-o ./tetgenAIM.o
g++ -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I/home/jenkins/util/tetgen/tetgen1.6.0 -I../utils \
-DTETLIBRARY tetgen_Interface.cpp -o ./tetgen_Interface.o
g++ -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DTETLIBRARY -w /home/jenkins/util/tetgen/tetgen1.6.0/tetgen.cxx -o ./tetgen.o
g++ -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -O0 -w /home/jenkins/util/tetgen/tetgen1.6.0/predicates.cxx -o ./predicates.o
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tetgenAIM.so ./tetgenAIM.o \
./tetgen_Interface.o ./tetgen.o \
./predicates.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -ldl -lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tetgen'
make -C tacs
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tacs'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils tacsAIM.c \
-o ./tacsAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tacsAIM.so ./tacsAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tacs'
make -C astros
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/astros'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils astrosAIM.c \
-o ./astrosAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils astrosUtils.c \
-o ./astrosUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils astrosCards.c \
-o ./astrosCards.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/astrosAIM.so ./astrosAIM.o ./astrosUtils.o ./astrosCards.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/astros'
make -C pointwise
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/pointwise'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils pointwiseAIM.c \
-o ./pointwiseAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils hashElement.c \
-o ./hashElement.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pointwiseAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pointwiseAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pointwiseAIM.so ./pointwiseAIM.o ./hashElement.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm -lpthread
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/pointwise'
make -C xfoil
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/xfoil'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
xfoilAIM.c -o ./xfoilAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/xfoilAIM.so ./xfoilAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/xfoil'
make -C aflr2
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr2'
Not compiling aflr2AIM: AFLR must be set -- Please fix the environment....
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr2'
make -C aflr4
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr4'
Not compiling aflr4AIM: AFLR must be set -- Please fix the environment....
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr4'
make -C su2
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/su2'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../meshWriter/su2Writer -I../utils su2AIM.c \
-o ./su2AIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2Utils.c \
-o ./su2Utils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_4_Cardinal.c \
-o ./su2_4_Cardinal.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_5_Raven.c \
-o ./su2_5_Raven.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_6_Falcon.c \
-o ./su2_6_Falcon.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_7_Blackbird.c \
-o ./su2_7_Blackbird.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_801_Harrier.c \
-o ./su2_801_Harrier.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/su2AIM.so ./su2AIM.o ./su2Utils.o ./su2_4_Cardinal.o ./su2_5_Raven.o ./su2_6_Falcon.o ./su2_7_Blackbird.o ./su2_801_Harrier.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/su2'
make -C cgt
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cgt'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include egads2cgt.c \
-o ./egads2cgt.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include aflr4egads.c \
-o ./aflr4egads.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/egads2cgt ./egads2cgt.o ./aflr4egads.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads -lcaps -locsm -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cgt'
make -C mses
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/mses'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils msesAIM.c -o msesAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils msesUtils.c -o msesUtils.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/msesAIM.so ./msesAIM.o ./msesUtils.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/mses'
make -C egadsTess
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/egadsTess'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils egadsTessAIM.c \
-o ./egadsTessAIM.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/egadsTessAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/egadsTessAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/egadsTessAIM.so ./egadsTessAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/egadsTess'
make -C sierraSD
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/sierraSD'
Not compiling sierraSDAIM: SEACAS must be set -- Please fix the environment....
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/sierraSD'
make -C masstran
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/masstran'
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils masstranAIM.cpp \
-o ./masstranAIM.o
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/masstranAIM.so ./masstranAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/masstran'
make -C plato
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/plato'
Not compiling platoAIM: SEACAS must be set -- Please fix the environment....
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/plato'
make -C refine
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/refine'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/libmeshbWriter refineAIM.c \
-o ./refineAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 \
-I../meshWriter/libmeshbWriter/libMeshb/sources \
../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \
-o ./libmeshb7.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/refineAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/refineAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/refineAIM.so ./refineAIM.o ./libmeshb7.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/refine'
make -C awave
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/awave'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils awaveAIM.c \
-o ./awaveAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/awaveAIM.so ./awaveAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/awave'
make -C tsfoil
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tsfoil'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
tsfoilAIM.c -o ./tsfoilAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tsfoilAIM.so ./tsfoilAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tsfoil'
make -C delaundo
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/delaundo'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils delaundoAIM.c \
-o ./delaundoAIM.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/delaundoAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/delaundoAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/delaundoAIM.so ./delaundoAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/delaundo'
make -C abaqus
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/abaqus'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
abaqusAIM.c -o ./abaqusAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
abaqusUtils.c -o ./abaqusUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
-I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/abaqusFILReader.c -o ./abaqusFILReader.o
echo "Building Abaqus with Python"
Building Abaqus with Python
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/abaqusAIM.so ./abaqusAIM.o ./abaqusUtils.o ./abaqusFILReader.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lm -ldl -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/abaqus'
make -C fun3d
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/fun3d'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \
-I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython fun3dAIM.c -o ./fun3dAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \
fun3dUtils.c -o ./fun3dUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
-I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/fun3dNamelist.c -o ./fun3dNamelist.o
Building FUN3D with Python
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fun3dAIM.so ./fun3dAIM.o ./fun3dUtils.o \
./fun3dNamelist.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -ldl -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lm -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/fun3d'
make -C cbaero
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cbaero'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o cbaeroAIM.o
gcc -g -shared -Wl,-no-undefined cbaeroAIM.o -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/cbaeroAIM.so -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cbaero'
make -C interference
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/interference'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include interferenceAIM.c \
-o ./interferenceAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. cloudFns.c \
-o ./cloudFns.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/interferenceAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/interferenceAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/interferenceAIM.so \
./interferenceAIM.o ./cloudFns.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib \
-laimUtil -locsm -legads -ludunits2 -ldl -lstdc++ -lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/interference'
make -C meshWriter
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter'
make -C libmeshbWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/libmeshbWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include libmeshbWriter.c \
-o ./libmeshbWriter.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -IlibMeshb/sources -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include libMeshb/sources/libmeshb7.c \
-o ./libmeshb7.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libmeshbWriter.so ./libmeshbWriter.o ./libmeshb7.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/libmeshbWriter'
make -C fastWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/fastWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include fastWriter.c \
-o ./fastWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fastWriter.so ./fastWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/fastWriter'
make -C tecplotWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/tecplotWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include tecplotWriter.c \
-o ./tecplotWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tecplotWriter.so ./tecplotWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/tecplotWriter'
make -C vtkWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/vtkWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include vtkWriter.c \
-o ./vtkWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vtkWriter.so ./vtkWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/vtkWriter'
make -C bstlWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bstlWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include bstlWriter.c \
-o ./bstlWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bstlWriter.so ./bstlWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bstlWriter'
make -C bvtkWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bvtkWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include bvtkWriter.c \
-o ./bvtkWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bvtkWriter.so ./bvtkWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bvtkWriter'
make -C su2Writer
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/su2Writer'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include su2Writer.c \
-o ./su2Writer.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/su2Writer.so ./su2Writer.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/su2Writer'
make -C stlWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/stlWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include stlWriter.c \
-o ./stlWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stlWriter.so ./stlWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/stlWriter'
make -C ugridWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/ugridWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include ugridWriter.c \
-o ./ugridWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ugridWriter.so ./ugridWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/ugridWriter'
make -C exodusWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/exodusWriter'
make[3]: Nothing to be done for `default'.
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/exodusWriter'
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter'
make -C cart3d
make[2]: xml2-config: Command not found
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cart3d'
XML developer libarary missing. Not compiling cart3dAIM.
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cart3d'
make -C nastran
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/nastran'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils nastranAIM.c \
-o ./nastranAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nastranAIM.so ./nastranAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/nastran'
make -C spinnaker
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/spinnaker'
make[2]: Nothing to be done for `default'.
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/spinnaker'
make -C aflr3
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr3'
Not compiling aflr3AIM: AFLR must be set -- Please fix the environment....
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr3'
make -C sierraSM
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/sierraSM'
Not compiling sierraSMAIM: SEACAS must be set -- Please fix the environment....
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/sierraSM'
make -C hsm
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils hsmAIM.c \
-o src/hsmAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils hsmUtils.c \
-o src/hsmUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils hsmAdj.c \
-o src/hsmAdj.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -Wno-comment rcm/rcm.cpp -DREVISION=7.8 \
-o src/rcm.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 rcm/genrcmi.cpp -DREVISION=7.8 \
-o src/genrcmi.o
make -C src hsmglr.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmglr.f -o ./hsmglr.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmbc.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbc.f -o ./hsmbc.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmbb2.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbb2.f -o ./hsmbb2.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmre1.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmre1.f -o ./hsmre1.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmdep.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmdep.f -o ./hsmdep.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmrfm.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmrfm.f -o ./hsmrfm.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmout.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmout.f -o ./hsmout.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmren.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmren.f -o ./hsmren.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmprj.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmprj.f -o ./hsmprj.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src atanc.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero atanc.f -o ./atanc.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src cross.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero cross.f -o ./cross.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src ludcmp.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero ludcmp.f -o ./ludcmp.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmabd.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmabd.f -o ./hsmabd.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src bmdump.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero bmdump.f -o ./bmdump.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmrun.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero -fno-recursive hsmrun.f -o ./hsmrun.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmeqn.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmeqn.f -o ./hsmeqn.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmsol.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmsol.f -o ./hsmsol.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmgeo.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmgeo.f -o ./hsmgeo.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src sbsolve.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero sbsolve.f -o ./sbsolve.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a hsmsol.o hsmdep.o hsmout.o hsmgeo.o hsmabd.o hsmeqn.o hsmbc.o hsmprj.o hsmren.o hsmre1.o hsmrfm.o hsmbb2.o hsmglr.o ludcmp.o sbsolve.o atanc.o bmdump.o cross.o )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hsmAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hsmAIM.so
gfortran -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hsmAIM.so \
src/hsmAIM.o src/hsmUtils.o src/hsmAdj.o \
src/rcm.o src/genrcmi.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -lhsm -ldl -lstdc++
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm'
make -C avl
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/avl'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils avlAIM.c -o ./avlAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o avlRead_ELE.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o avlRead_DERMATB.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o avlRead_HINGE.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o avlRead_BODY.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o avlRead_CNC.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o avlRead_TOT.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o avlRead_DERMATS.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o avlRead_STRP.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o avlRead_VM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o avlRead_CPOML.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o avlRead_DERMATM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o avlRead_SURF.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/avlAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/avlAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/avlAIM.so ./avlAIM.o ./avlRead_ELE.o ./avlRead_DERMATB.o ./avlRead_HINGE.o ./avlRead_BODY.o ./avlRead_CNC.o ./avlRead_TOT.o ./avlRead_DERMATS.o ./avlRead_STRP.o ./avlRead_VM.o ./avlRead_CPOML.o ./avlRead_DERMATM.o ./avlRead_SURF.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \
-lstdc++ -lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/avl'
make -C custom
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/custom'
make[2]: Nothing to be done for `default'.
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/custom'
make -C skeleton
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/skeleton'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils skeletonAIM.c \
-o ./skeletonAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/skeletonAIM.so ./skeletonAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/skeleton'
make -C unitTest
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest'
make[2]: Nothing to be done for `all'.
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest'
make -C mystran
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/mystran'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils mystranAIM.c \
-o ./mystranAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils mystranUtils.c \
-o ./mystranUtils.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mystranAIM.so ./mystranAIM.o ./mystranUtils.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/mystran'
make -C zaero
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/zaero'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroAIM.c -o zaeroAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroUtils.c -o zaeroUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroLinearFlutter.c -o zaeroLinearFlutter.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroTrim.c -o zaeroTrim.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroTypes.c -o zaeroTypes.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroCards.c -o zaeroCards.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroGeneral.c -o zaeroGeneral.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroGraphical.c -o zaeroGraphical.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/zaeroAIM.so ./zaeroAIM.o ./zaeroUtils.o ./zaeroLinearFlutter.o ./zaeroTrim.o ./zaeroTypes.o ./zaeroCards.o ./zaeroGeneral.o ./zaeroGraphical.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/zaero'
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim'
(cd OpenCSM; make -f serveESP.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/OpenCSM'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timCapsMode.c -o ./timCapsMode.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/capsMode.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/capsMode.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/capsMode.so ./timCapsMode.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timFlowchart.c -o ./timFlowchart.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flowchart.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flowchart.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flowchart.so ./timFlowchart.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timViewer.c -o ./timViewer.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/viewer.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/viewer.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/viewer.so ./timViewer.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 timPyscript.c -o ./timPyscript.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pyscript.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pyscript.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pyscript.so ./timPyscript.o -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lrt -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/OpenCSM'
*** Build Completed! ***
+ export CSMDATA=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data
+ CSMDATA=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin
++ uname -a
+ [[ Linux reynolds-centOS7 3.10.0-1160.108.1.el7.x86_64 #1 SMP Thu Jan 25 16:17:31 UTC 2024 x86_64 x86_64 x86_64 GNU/Linux == *\D\a\r\w\i\n* ]]
+ sed -i 's/.*capsExamples.*/#&/' /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/Verification.sh
+ bash -ex /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/Verification.sh
+ expectSuccess 01 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/expressions.vfy", so verification is being skipped
ERROR:: 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 0m0.141s
user 0m0.089s
sys 0m0.048s
+ set +x
=============================================
ESP verification case 01 passed (as expected)
=============================================
+ expectSuccess 02 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/demo2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/demo2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/demo2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.381s
user 0m0.372s
sys 0m0.026s
+ set +x
=============================================
ESP verification case 02 passed (as expected)
=============================================
+ expectSuccess 03 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial1_whole
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial1_whole
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/verify_7.8.0/tutorial1_whole.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m2.928s
user 0m3.827s
sys 0m0.045s
+ set +x
=============================================
ESP verification case 03 passed (as expected)
=============================================
+ expectSuccess 04 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/design2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/design2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/design2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.718s
user 0m0.723s
sys 0m0.038s
+ set +x
=============================================
ESP verification case 04 passed (as expected)
=============================================
+ expectSuccess 05 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/design3
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/design3
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/design3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.606s
user 0m0.786s
sys 0m0.025s
+ set +x
=============================================
ESP verification case 05 passed (as expected)
=============================================
+ expectSuccess 06 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/verify_7.8.0/tutorial2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.620s
user 0m0.785s
sys 0m0.034s
+ set +x
=============================================
ESP verification case 06 passed (as expected)
=============================================
+ expectSuccess 07 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial3
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial3
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/verify_7.8.0/tutorial3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m3.567s
user 0m5.323s
sys 0m0.148s
+ set +x
=============================================
ESP verification case 07 passed (as expected)
=============================================
+ expectSuccess 08 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/CAPS/myPlane
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/CAPS/myPlane
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/CAPS/verify_7.8.0/myPlane.vfy", so verification is being skipped
==> serveESP completed successfully with 12 warnings and no verification data
real 0m31.025s
user 0m46.495s
sys 0m0.628s
+ set +x
=============================================
ESP verification case 08 passed (as expected)
=============================================
+ expectSuccess 09 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/bottle
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/bottle
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/verify_7.8.0/bottle.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.670s
user 0m0.976s
sys 0m0.032s
+ set +x
=============================================
ESP verification case 09 passed (as expected)
=============================================
+ expectSuccess 10 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/wingMultiModel
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/wingMultiModel
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/wingMultiModel.vfy", so verification is being skipped
==> serveESP completed successfully with 4 warnings and no verification data
real 0m36.825s
user 1m1.081s
sys 0m1.078s
+ set +x
=============================================
ESP verification case 10 passed (as expected)
=============================================
+ expectSuccess 11 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/bullet
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/bullet
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/bullet.vfy", so verification is being skipped
WARNING:: 8 _hist and/or __trace__ attributes removed
WARNING:: 8 _hist and/or __trace__ attributes removed
WARNING:: could not find mapping for iedge=10
WARNING:: could not find mapping for iedge=14
WARNING:: could not find mapping for iedge=7
WARNING:: could not find mapping for iedge=11
==> serveESP completed successfully with 5 warnings and no verification data
real 0m0.313s
user 0m0.289s
sys 0m0.031s
+ set +x
=============================================
ESP verification case 11 passed (as expected)
=============================================
+ expectSuccess 12 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/connect5
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/connect5
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/connect5.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.578s
user 0m0.888s
sys 0m0.013s
+ set +x
=============================================
ESP verification case 12 passed (as expected)
=============================================
+ expectSuccess 13 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/group2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/group2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/group2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.182s
user 0m0.163s
sys 0m0.020s
+ set +x
=============================================
ESP verification case 13 passed (as expected)
=============================================
+ expectSuccess 14 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/csm3
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/csm3
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/csm3.vfy", so verification is being skipped
nnode=8
nedge=12
nface=6
nnode=8
nedge=12
nface=6
nnode=16
nedge=24
nface=10
nnode=8
nedge=12
nface=6
==> serveESP completed successfully with no verification data
real 0m0.462s
user 0m0.465s
sys 0m0.015s
+ set +x
=============================================
ESP verification case 14 passed (as expected)
=============================================
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/testEGADS
+ make test
python --version
Python 3.11.9
python -u -m unittest discover
.................................................... PCurve Map: 48 (alloc 48)!
Surface Map: 12 (alloc 24)!
Curve Map: 28 (alloc 28)!
Writing PCurves...
Writing Curves...
Writing Surfaces...
Writing 16 Nodes...
Writing 28 Edges...
Writing 12 Loops...
Writing 12 Faces...
Writing 1 Shells...
EGADS Info: 0 Objects, 0 Reference in Use (of 972) at Close!
...................
----------------------------------------------------------------------
Ran 71 tests in 2.146s
OK
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/testOCSM
+ source /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/test_pyOCSM.sh
++ set -x
++ python -u test_pyOCSM.py -skipHelp
real 0m5.930s
user 0m10.589s
sys 0m0.145s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/testCAPS
+ make test
python --version
Python 3.11.9
python -u -m unittest discover
..Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing1, index = 1
Name = Wing2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 143
Number of elements = 282
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 282
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 140
Number of elements = 276
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 276
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 283
Combined Number of elements = 558
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 558
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Wing1
Property name - Wing2
Done getting FEA properties
Updating mesh element types based on properties input
... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
..Writing D3 Javascript library - d3.v3.min.js
........... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing1, index = 1
Name = Wing2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 209
Number of elements = 414
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 414
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 186
Number of elements = 368
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 368
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 395
Combined Number of elements = 782
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 782
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Wing1
Property name - Wing2
Done getting FEA properties
Updating mesh element types based on properties input
..........--> Opening DESPMTR file "unitGeom.param"
updating CFGPMTR series [ 1, 1] = 8412.000000
updating CFGPMTR series2 [ 1, 1] = 20.000000
updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000
updating CFGPMTR nrow [ 1, 1] = 3.000000
updating CFGPMTR ncol [ 1, 1] = 2.000000
updating DESPMTR area [ 1, 1] = 40.000000
updating DESPMTR aspect [ 1, 1] = 5.000000
updating DESPMTR taper [ 1, 1] = 0.500000
updating DESPMTR twist [ 1, 1] = 15.000000
updating DESPMTR wing:lesweep [ 1, 1] = 30.000000
updating DESPMTR wing:dihedral [ 1, 1] = 1.000000
updating DESPMTR wing:chord:root [ 1, 1] = 1.560000
updating DESPMTR htail [ 1, 1] = 1.000000
updating DESPMTR htail:chord [ 1, 1] = 2.000000
updating DESPMTR vtail:chord [ 1, 1] = 3.000000
updating DESPMTR vtail [ 1, 1] = 4.000000
updating DESPMTR sphereR [ 1, 1] = 80.000000
updating DESPMTR v@1:d_name [ 1, 1] = 1.000000
updating DESPMTR despMat [ 1, 1] = 11.000000
updating DESPMTR despMat [ 1, 2] = 12.000000
updating DESPMTR despMat [ 2, 1] = 13.000000
updating DESPMTR despMat [ 2, 2] = 14.000000
updating DESPMTR despMat [ 3, 1] = 15.000000
updating DESPMTR despMat [ 3, 2] = 16.000000
updating DESPMTR despCol [ 1, 1] = 11.000000
updating DESPMTR despCol [ 2, 1] = 13.000000
updating DESPMTR despCol [ 3, 1] = 15.000000
updating DESPMTR despRow [ 1, 1] = 11.000000
updating DESPMTR despRow [ 1, 2] = 12.000000
updating DESPMTR despRow [ 1, 3] = 13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
..Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
No linkable data found for Altitude
No linkable data found for Strings
No linkable data found for Strings2
Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
............ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. CAPS Info: Hit last success -- going live!
... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.--> Opening DESPMTR file "unitGeom.param"
updating CFGPMTR series [ 1, 1] = 8412.000000
updating CFGPMTR series2 [ 1, 1] = 20.000000
updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000
updating CFGPMTR nrow [ 1, 1] = 3.000000
updating CFGPMTR ncol [ 1, 1] = 2.000000
updating DESPMTR area [ 1, 1] = 40.000000
updating DESPMTR aspect [ 1, 1] = 5.000000
updating DESPMTR taper [ 1, 1] = 0.500000
updating DESPMTR twist [ 1, 1] = 15.000000
updating DESPMTR wing:lesweep [ 1, 1] = 30.000000
updating DESPMTR wing:dihedral [ 1, 1] = 1.000000
updating DESPMTR wing:chord:root [ 1, 1] = 1.560000
updating DESPMTR htail [ 1, 1] = 1.000000
updating DESPMTR htail:chord [ 1, 1] = 2.000000
updating DESPMTR vtail:chord [ 1, 1] = 3.000000
updating DESPMTR vtail [ 1, 1] = 4.000000
updating DESPMTR sphereR [ 1, 1] = 80.000000
updating DESPMTR v@1:d_name [ 1, 1] = 1.000000
updating DESPMTR despMat [ 1, 1] = 11.000000
updating DESPMTR despMat [ 1, 2] = 12.000000
updating DESPMTR despMat [ 2, 1] = 13.000000
updating DESPMTR despMat [ 2, 2] = 14.000000
updating DESPMTR despMat [ 3, 1] = 15.000000
updating DESPMTR despMat [ 3, 2] = 16.000000
updating DESPMTR despCol [ 1, 1] = 11.000000
updating DESPMTR despCol [ 2, 1] = 13.000000
updating DESPMTR despCol [ 3, 1] = 15.000000
updating DESPMTR despRow [ 1, 1] = 11.000000
updating DESPMTR despRow [ 1, 2] = 12.000000
updating DESPMTR despRow [ 1, 3] = 13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
................ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
----------------------------------------------------------------------
Ran 100 tests in 12.253s
OK
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/
+ make test
python --version
Python 3.11.9
python -u -m unittest discover --verbose
Please set the environment variable ASTROS_ROOT
test_journal (test_aflr2.TestAFLR2.test_journal) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 04/23/24 @ 12:17PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2244 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2244 2244
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 450 902
AFLR2 IG : Nodes, Faces = 900 1802
AFLR2 IG : Nodes, Faces = 1145 2292
AFLR2 IG : Nodes, Faces = 1260 2522
AFLR2 IG : Nodes, Faces = 1350 2702
AFLR2 IG : Nodes, Faces = 1360 2722
AFLR2 IG : Nodes, Faces = 1460 2922
AFLR2 IG : Nodes, Faces = 1560 3122
AFLR2 IG : Nodes, Faces = 1660 3322
AFLR2 IG : Nodes, Faces = 1760 3522
AFLR2 IG : Nodes, Faces = 1800 3602
AFLR2 IG : Nodes, Faces = 1860 3722
AFLR2 IG : Nodes, Faces = 1960 3922
AFLR2 IG : Nodes, Faces = 2060 4122
AFLR2 IG : Nodes, Faces = 2085 4172
AFLR2 IG : Nodes, Faces = 2244 4490
AFLR2 IG : Nodes, Faces = 2248 4490
AFLR2 IG : Nodes, Faces = 2244 2244
AFLR2 : CPU Time = 0.032 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 = 0.008 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
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 = 0.038 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 = 0.133 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.007 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2244 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2244 2244
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 450 902
AFLR2 IG : Nodes, Faces = 900 1802
AFLR2 IG : Nodes, Faces = 1145 2292
AFLR2 IG : Nodes, Faces = 1260 2522
AFLR2 IG : Nodes, Faces = 1350 2702
AFLR2 IG : Nodes, Faces = 1360 2722
AFLR2 IG : Nodes, Faces = 1460 2922
AFLR2 IG : Nodes, Faces = 1560 3122
AFLR2 IG : Nodes, Faces = 1660 3322
AFLR2 IG : Nodes, Faces = 1760 3522
AFLR2 IG : Nodes, Faces = 1800 3602
AFLR2 IG : Nodes, Faces = 1860 3722
AFLR2 IG : Nodes, Faces = 1960 3922
AFLR2 IG : Nodes, Faces = 2060 4122
AFLR2 IG : Nodes, Faces = 2085 4172
AFLR2 IG : Nodes, Faces = 2244 4490
AFLR2 IG : Nodes, Faces = 2248 4490
AFLR2 IG : Nodes, Faces = 2244 2244
AFLR2 : CPU Time = 0.032 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 = 0.101 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.007 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2224 0
AFLR2 : CPU Time = 0.001 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 = 0.029 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2224 2224
AFLR2 GG : Nodes, Faces = 4122 6020
AFLR2 GG : Nodes, Faces = 5812 9400
AFLR2 GG : Nodes, Faces = 7299 12374
AFLR2 GG : Nodes, Faces = 8574 14924
AFLR2 GG : Nodes, Faces = 9729 17234
AFLR2 GG : Nodes, Faces = 10787 19350
AFLR2 GG : Nodes, Faces = 11767 21310
AFLR2 GG : Nodes, Faces = 12683 23142
AFLR2 GG : Nodes, Faces = 13516 24808
AFLR2 GG : Nodes, Faces = 14278 26332
AFLR2 GG : Nodes, Faces = 14999 27774
AFLR2 GG : Nodes, Faces = 15682 29140
AFLR2 GG : Nodes, Faces = 16312 30400
AFLR2 GG : Nodes, Faces = 16899 31574
AFLR2 GG : Nodes, Faces = 17451 32678
AFLR2 GG : Nodes, Faces = 17959 33694
AFLR2 GG : Nodes, Faces = 18443 34662
AFLR2 GG : Nodes, Faces = 18877 35530
AFLR2 GG : Nodes, Faces = 19283 36342
AFLR2 GG : Nodes, Faces = 19650 37076
AFLR2 GG : Nodes, Faces = 19994 37764
AFLR2 GG : Nodes, Faces = 20325 38426
AFLR2 GG : Nodes, Faces = 20638 39052
AFLR2 GG : Nodes, Faces = 20940 39656
AFLR2 GG : Nodes, Faces = 21240 40256
AFLR2 GG : Nodes, Faces = 21523 40822
AFLR2 GG : Nodes, Faces = 21792 41360
AFLR2 GG : Nodes, Faces = 22053 41882
AFLR2 GG : Nodes, Faces = 22305 42386
AFLR2 GG : Nodes, Faces = 22521 42818
AFLR2 GG : Nodes, Faces = 22696 43168
AFLR2 GG : Nodes, Faces = 22829 43434
AFLR2 GG : Nodes, Faces = 22953 43682
AFLR2 GG : Nodes, Faces = 23050 43876
AFLR2 GG : Nodes, Faces = 23110 43996
AFLR2 GG : Nodes, Faces = 23139 44054
AFLR2 GG : Nodes, Faces = 23157 44090
AFLR2 GG : Nodes, Faces = 23175 44126
AFLR2 GG : Nodes, Faces = 23183 44142
AFLR2 GG : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.106 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.028 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 = 0.111 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.009 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 48 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 48 48
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 10 22
AFLR2 IG : Nodes, Faces = 20 42
AFLR2 IG : Nodes, Faces = 30 62
AFLR2 IG : Nodes, Faces = 40 82
AFLR2 IG : Nodes, Faces = 45 92
AFLR2 IG : Nodes, Faces = 46 94
AFLR2 IG : Nodes, Faces = 48 98
AFLR2 IG : Nodes, Faces = 52 98
AFLR2 IG : Nodes, Faces = 48 48
AFLR2 : CPU Time = 0.000 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 48 48
AFLR2 GG : Nodes, Faces = 88 128
AFLR2 GG : Nodes, Faces = 109 170
AFLR2 GG : Nodes, Faces = 124 200
AFLR2 GG : Nodes, Faces = 136 224
AFLR2 GG : Nodes, Faces = 148 248
AFLR2 GG : Nodes, Faces = 161 274
AFLR2 GG : Nodes, Faces = 171 294
AFLR2 GG : Nodes, Faces = 181 314
AFLR2 GG : Nodes, Faces = 187 326
AFLR2 GG : Nodes, Faces = 190 332
AFLR2 : CPU Time = 0.000 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 190 332
AFLR2 : CPU Time = 0.000 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 190
Number of elements = 380
Number of tris = 332
Number of quad = 0
ok
test_reenter (test_aflr2.TestAFLR2.test_reenter) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 339 680
AFLR2 IG : Nodes, Faces = 340 682
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.001 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 344 344
AFLR2 GG : Nodes, Faces = 679 1014
AFLR2 GG : Nodes, Faces = 1006 1668
AFLR2 GG : Nodes, Faces = 1321 2298
AFLR2 GG : Nodes, Faces = 1604 2864
AFLR2 GG : Nodes, Faces = 1886 3428
AFLR2 GG : Nodes, Faces = 2155 3966
AFLR2 GG : Nodes, Faces = 2409 4474
AFLR2 GG : Nodes, Faces = 2649 4954
AFLR2 GG : Nodes, Faces = 2867 5390
AFLR2 GG : Nodes, Faces = 3063 5782
AFLR2 GG : Nodes, Faces = 3243 6142
AFLR2 GG : Nodes, Faces = 3400 6456
AFLR2 GG : Nodes, Faces = 3540 6736
AFLR2 GG : Nodes, Faces = 3665 6986
AFLR2 GG : Nodes, Faces = 3786 7228
AFLR2 GG : Nodes, Faces = 3900 7456
AFLR2 GG : Nodes, Faces = 4010 7676
AFLR2 GG : Nodes, Faces = 4114 7884
AFLR2 GG : Nodes, Faces = 4209 8074
AFLR2 GG : Nodes, Faces = 4292 8240
AFLR2 GG : Nodes, Faces = 4368 8392
AFLR2 GG : Nodes, Faces = 4439 8534
AFLR2 GG : Nodes, Faces = 4503 8662
AFLR2 GG : Nodes, Faces = 4560 8776
AFLR2 GG : Nodes, Faces = 4611 8878
AFLR2 GG : Nodes, Faces = 4650 8956
AFLR2 GG : Nodes, Faces = 4677 9010
AFLR2 GG : Nodes, Faces = 4695 9046
AFLR2 GG : Nodes, Faces = 4705 9066
AFLR2 : CPU Time = 0.009 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 4705 9066
AFLR2 : CPU Time = 0.001 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 4705
Number of elements = 9410
Number of tris = 9066
Number of quad = 0
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates!
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 339 680
AFLR2 IG : Nodes, Faces = 340 682
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.001 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 344 344
AFLR2 GGp: Nodes, Faces = 682 1020
AFLR2 GGp: Nodes, Faces = 1010 1676
AFLR2 GGp: Nodes, Faces = 1316 2288
AFLR2 GGp: Nodes, Faces = 1592 2840
AFLR2 GGp: Nodes, Faces = 1855 3366
AFLR2 GGp: Nodes, Faces = 2106 3868
AFLR2 GGp: Nodes, Faces = 2341 4338
AFLR2 GGp: Nodes, Faces = 2551 4758
AFLR2 GGp: Nodes, Faces = 2741 5138
AFLR2 GGp: Nodes, Faces = 2917 5490
AFLR2 GGp: Nodes, Faces = 3082 5820
AFLR2 GGp: Nodes, Faces = 3240 6136
AFLR2 GGp: Nodes, Faces = 3379 6414
AFLR2 GGp: Nodes, Faces = 3513 6682
AFLR2 GGp: Nodes, Faces = 3642 6940
AFLR2 GGp: Nodes, Faces = 3748 7152
AFLR2 GGp: Nodes, Faces = 3846 7348
AFLR2 GGp: Nodes, Faces = 3931 7518
AFLR2 GGp: Nodes, Faces = 3999 7654
AFLR2 GGp: Nodes, Faces = 4044 7744
AFLR2 GGp: Nodes, Faces = 4058 7772
AFLR2 : CPU Time = 0.011 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 = 0.006 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 4055
Number of elements = 4420
Number of tris = 386
Number of quad = 3690
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates!
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
ok
test_setInput (test_aflr2.TestAFLR2.test_setInput) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 339 680
AFLR2 IG : Nodes, Faces = 340 682
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.001 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 344 344
AFLR2 GGp: Nodes, Faces = 682 1020
AFLR2 GGp: Nodes, Faces = 1010 1676
AFLR2 GGp: Nodes, Faces = 1316 2288
AFLR2 GGp: Nodes, Faces = 1592 2840
AFLR2 GGp: Nodes, Faces = 1855 3366
AFLR2 GGp: Nodes, Faces = 2106 3868
AFLR2 GGp: Nodes, Faces = 2341 4338
AFLR2 GGp: Nodes, Faces = 2551 4758
AFLR2 GGp: Nodes, Faces = 2741 5138
AFLR2 GGp: Nodes, Faces = 2917 5490
AFLR2 GGp: Nodes, Faces = 3082 5820
AFLR2 GGp: Nodes, Faces = 3240 6136
AFLR2 GGp: Nodes, Faces = 3379 6414
AFLR2 GGp: Nodes, Faces = 3513 6682
AFLR2 GGp: Nodes, Faces = 3642 6940
AFLR2 GGp: Nodes, Faces = 3748 7152
AFLR2 GGp: Nodes, Faces = 3846 7348
AFLR2 GGp: Nodes, Faces = 3931 7518
AFLR2 GGp: Nodes, Faces = 3999 7654
AFLR2 GGp: Nodes, Faces = 4044 7744
AFLR2 GGp: Nodes, Faces = 4058 7772
AFLR2 : CPU Time = 0.011 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 = 0.006 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:62408)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box, index = 1
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 04/23/24 @ 12:17PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR4 : Compile Date 04/23/24 @ 12:17PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 7):
Number of nodes = 1189
Number of elements = 6249
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4917
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cylinder, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 7):
Number of nodes = 6092
Number of elements = 33723
Number of triangles = 4434
Number of quadrilatarals = 0
Number of tetrahedrals = 29289
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cone, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 7):
Number of nodes = 13578
Number of elements = 76165
Number of triangles = 8144
Number of quadrilatarals = 0
Number of tetrahedrals = 68021
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = torus, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 7):
Number of nodes = 42341
Number of elements = 240656
Number of triangles = 19890
Number of quadrilatarals = 0
Number of tetrahedrals = 220766
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = sphere, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 7):
Number of nodes = 4356
Number of elements = 24173
Number of triangles = 3018
Number of quadrilatarals = 0
Number of tetrahedrals = 21155
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = boxhole, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 7):
Number of nodes = 10984
Number of elements = 60667
Number of triangles = 8628
Number of quadrilatarals = 0
Number of tetrahedrals = 52039
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = bullet, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 7):
Number of nodes = 10678
Number of elements = 59894
Number of triangles = 6366
Number of quadrilatarals = 0
Number of tetrahedrals = 53528
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Getting volume mesh for body 1 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 89218
Number of elements = 501527
Number of triangles = 51812
Number of quadrilatarals = 0
Number of tetrahedrals = 449715
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_all (test_aflr3.TestAFLR3.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = farfield, index = 8
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = farfield, index = 8
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 16488
Number of elements = 93795
Number of triangles = 7926
Number of quadrilatarals = 0
Number of tetrahedrals = 85869
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_box (test_aflr3.TestAFLR3.test_box) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2589
Number of elements = 13809
Number of triangles = 2758
Number of quadrilatarals = 0
Number of tetrahedrals = 11051
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_boxhole (test_aflr3.TestAFLR3.test_boxhole) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3649
Number of elements = 19777
Number of triangles = 3394
Number of quadrilatarals = 0
Number of tetrahedrals = 16383
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_bullet (test_aflr3.TestAFLR3.test_bullet) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5514
Number of elements = 30658
Number of triangles = 3656
Number of quadrilatarals = 0
Number of tetrahedrals = 27002
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_cone (test_aflr3.TestAFLR3.test_cone) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4694
Number of elements = 25935
Number of triangles = 3326
Number of quadrilatarals = 0
Number of tetrahedrals = 22609
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_cylinder (test_aflr3.TestAFLR3.test_cylinder) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5554
Number of elements = 30862
Number of triangles = 3756
Number of quadrilatarals = 0
Number of tetrahedrals = 27106
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_faceMatch (test_aflr3.TestAFLR3.test_faceMatch) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2260
Number of elements = 12133
Number of triangles = 2222
Number of quadrilatarals = 0
Number of tetrahedrals = 9911
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2392
Number of elements = 12577
Number of triangles = 2666
Number of quadrilatarals = 0
Number of tetrahedrals = 9911
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3341
Number of elements = 18069
Number of triangles = 3110
Number of quadrilatarals = 0
Number of tetrahedrals = 14959
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3606
Number of elements = 18961
Number of triangles = 4002
Number of quadrilatarals = 0
Number of tetrahedrals = 14959
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4414
Number of elements = 23974
Number of triangles = 3998
Number of quadrilatarals = 0
Number of tetrahedrals = 19976
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4811
Number of elements = 25310
Number of triangles = 5334
Number of quadrilatarals = 0
Number of tetrahedrals = 19976
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 4):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 4):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 4):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 4):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5490
Number of elements = 29891
Number of triangles = 4886
Number of quadrilatarals = 0
Number of tetrahedrals = 25005
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6019
Number of elements = 31671
Number of triangles = 6666
Number of quadrilatarals = 0
Number of tetrahedrals = 25005
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 5):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 5):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 5):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 5):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 5):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6542
Number of elements = 35667
Number of triangles = 5774
Number of quadrilatarals = 0
Number of tetrahedrals = 29893
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 7203
Number of elements = 37891
Number of triangles = 7998
Number of quadrilatarals = 0
Number of tetrahedrals = 29893
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 6):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 6):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 6):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 6):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 6):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 6):
Number of nodes = 1184
Number of elements = 6220
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4888
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 7601
Number of elements = 41489
Number of triangles = 6662
Number of quadrilatarals = 0
Number of tetrahedrals = 34827
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8394
Number of elements = 44157
Number of triangles = 9330
Number of quadrilatarals = 0
Number of tetrahedrals = 34827
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 7):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 7):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 7):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 7):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 7):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 7):
Number of nodes = 1184
Number of elements = 6220
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4888
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 7):
Number of nodes = 1191
Number of elements = 6266
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4934
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 19800
Number of elements = 109798
Number of triangles = 15540
Number of quadrilatarals = 0
Number of tetrahedrals = 94258
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 8 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 9 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 10 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 11 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 12 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 13 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 14 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 15 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 16 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 17 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 18 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 19 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 22741
Number of elements = 119570
Number of triangles = 25312
Number of quadrilatarals = 0
Number of tetrahedrals = 94258
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 19):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 19):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 19):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 19):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 19):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 19):
Number of nodes = 1184
Number of elements = 6220
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4888
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 19):
Number of nodes = 1191
Number of elements = 6266
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4934
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 8 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 8 (of 19):
Number of nodes = 1193
Number of elements = 6272
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4940
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 9 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 9 (of 19):
Number of nodes = 1176
Number of elements = 6165
Number of triangles = 1330
Number of quadrilatarals = 0
Number of tetrahedrals = 4835
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 10 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 10 (of 19):
Number of nodes = 1203
Number of elements = 6314
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4982
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 11 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 11 (of 19):
Number of nodes = 1192
Number of elements = 6269
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4937
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 12 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 12 (of 19):
Number of nodes = 1192
Number of elements = 6269
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4937
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 13 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 13 (of 19):
Number of nodes = 1198
Number of elements = 6296
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4964
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 14 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 14 (of 19):
Number of nodes = 1223
Number of elements = 6443
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5111
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 15 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 15 (of 19):
Number of nodes = 1184
Number of elements = 6224
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4892
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 16 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 16 (of 19):
Number of nodes = 1195
Number of elements = 6287
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4955
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 17 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 17 (of 19):
Number of nodes = 1197
Number of elements = 6311
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4979
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 18 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 18 (of 19):
Number of nodes = 1203
Number of elements = 6310
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4978
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 19 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 19 (of 19):
Number of nodes = 1191
Number of elements = 6253
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4921
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_faceMatch_MultiDomain (test_aflr3.TestAFLR3.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8857
Number of elements = 49191
Number of triangles = 6284
Number of quadrilatarals = 0
Number of tetrahedrals = 42907
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8989
Number of elements = 49635
Number of triangles = 6728
Number of quadrilatarals = 0
Number of tetrahedrals = 42907
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 7796
Number of elements = 43368
Number of triangles = 5396
Number of quadrilatarals = 0
Number of tetrahedrals = 37972
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 1193
Number of elements = 6267
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4935
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9944
Number of elements = 55193
Number of triangles = 7174
Number of quadrilatarals = 0
Number of tetrahedrals = 48019
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10218
Number of elements = 56081
Number of triangles = 8062
Number of quadrilatarals = 0
Number of tetrahedrals = 48019
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7818
Number of elements = 43469
Number of triangles = 5398
Number of quadrilatarals = 0
Number of tetrahedrals = 38071
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1202
Number of elements = 6320
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4988
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 1198
Number of elements = 6292
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4960
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9609
Number of elements = 53228
Number of triangles = 6994
Number of quadrilatarals = 0
Number of tetrahedrals = 46234
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9829
Number of elements = 53956
Number of triangles = 7722
Number of quadrilatarals = 0
Number of tetrahedrals = 46234
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7789
Number of elements = 43295
Number of triangles = 5394
Number of quadrilatarals = 0
Number of tetrahedrals = 37901
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1186
Number of elements = 6230
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4898
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 854
Number of elements = 4431
Number of triangles = 996
Number of quadrilatarals = 0
Number of tetrahedrals = 3435
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9348
Number of elements = 51734
Number of triangles = 6812
Number of quadrilatarals = 0
Number of tetrahedrals = 44922
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9531
Number of elements = 52330
Number of triangles = 7408
Number of quadrilatarals = 0
Number of tetrahedrals = 44922
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7804
Number of elements = 43358
Number of triangles = 5386
Number of quadrilatarals = 0
Number of tetrahedrals = 37972
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1200
Number of elements = 6311
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4979
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 527
Number of elements = 2661
Number of triangles = 690
Number of quadrilatarals = 0
Number of tetrahedrals = 1971
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9183
Number of elements = 50871
Number of triangles = 6632
Number of quadrilatarals = 0
Number of tetrahedrals = 44239
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9322
Number of elements = 51307
Number of triangles = 7068
Number of quadrilatarals = 0
Number of tetrahedrals = 44239
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7927
Number of elements = 44116
Number of triangles = 5382
Number of quadrilatarals = 0
Number of tetrahedrals = 38734
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 868
Number of elements = 4530
Number of triangles = 996
Number of quadrilatarals = 0
Number of tetrahedrals = 3534
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 527
Number of elements = 2661
Number of triangles = 690
Number of quadrilatarals = 0
Number of tetrahedrals = 1971
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10181
Number of elements = 56797
Number of triangles = 6782
Number of quadrilatarals = 0
Number of tetrahedrals = 50015
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10671
Number of elements = 58561
Number of triangles = 8546
Number of quadrilatarals = 0
Number of tetrahedrals = 50015
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7741
Number of elements = 43010
Number of triangles = 5362
Number of quadrilatarals = 0
Number of tetrahedrals = 37648
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 2692
Number of elements = 14435
Number of triangles = 2800
Number of quadrilatarals = 0
Number of tetrahedrals = 11635
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 238
Number of elements = 1116
Number of triangles = 384
Number of quadrilatarals = 0
Number of tetrahedrals = 732
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1500
Number of elements = 7757
Number of triangles = 1986
Number of quadrilatarals = 0
Number of tetrahedrals = 5771
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1564
Number of elements = 7881
Number of triangles = 2110
Number of quadrilatarals = 0
Number of tetrahedrals = 5771
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 1160
Number of elements = 6087
Number of triangles = 1308
Number of quadrilatarals = 0
Number of tetrahedrals = 4779
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 360
Number of elements = 1635
Number of triangles = 718
Number of quadrilatarals = 0
Number of tetrahedrals = 917
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 44
Number of elements = 159
Number of triangles = 84
Number of quadrilatarals = 0
Number of tetrahedrals = 75
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5092
Number of elements = 27888
Number of triangles = 4070
Number of quadrilatarals = 0
Number of tetrahedrals = 23818
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5238
Number of elements = 28440
Number of triangles = 4622
Number of quadrilatarals = 0
Number of tetrahedrals = 23818
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 4902
Number of elements = 26933
Number of triangles = 4038
Number of quadrilatarals = 0
Number of tetrahedrals = 22895
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 336
Number of elements = 1507
Number of triangles = 584
Number of quadrilatarals = 0
Number of tetrahedrals = 923
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 33106
Number of elements = 191761
Number of triangles = 8496
Number of quadrilatarals = 0
Number of tetrahedrals = 183265
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 36447
Number of elements = 205093
Number of triangles = 21828
Number of quadrilatarals = 0
Number of tetrahedrals = 183265
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 5):
Number of nodes = 28882
Number of elements = 164134
Number of triangles = 15162
Number of quadrilatarals = 0
Number of tetrahedrals = 148972
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 5):
Number of nodes = 1415
Number of elements = 7515
Number of triangles = 1456
Number of quadrilatarals = 0
Number of tetrahedrals = 6059
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 5):
Number of nodes = 4186
Number of elements = 23181
Number of triangles = 2942
Number of quadrilatarals = 0
Number of tetrahedrals = 20239
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 5):
Number of nodes = 711
Number of elements = 3685
Number of triangles = 844
Number of quadrilatarals = 0
Number of tetrahedrals = 2841
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 5):
Number of nodes = 1253
Number of elements = 6578
Number of triangles = 1424
Number of quadrilatarals = 0
Number of tetrahedrals = 5154
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 16786
Number of elements = 95215
Number of triangles = 8798
Number of quadrilatarals = 0
Number of tetrahedrals = 86417
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 18710
Number of elements = 102591
Number of triangles = 16174
Number of quadrilatarals = 0
Number of tetrahedrals = 86417
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 12124
Number of elements = 68112
Number of triangles = 7138
Number of quadrilatarals = 0
Number of tetrahedrals = 60974
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 6586
Number of elements = 34479
Number of triangles = 9036
Number of quadrilatarals = 0
Number of tetrahedrals = 25443
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_journal (test_aflr3.TestAFLR3.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2940
Number of elements = 12771
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7319
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2497
Number of elements = 10947
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6395
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2940
Number of elements = 12771
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7319
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2497
Number of elements = 10947
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6395
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
ok
test_phase (test_aflr3.TestAFLR3.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2940
Number of elements = 12771
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7319
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2497
Number of elements = 10947
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6395
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_reenter (test_aflr3.TestAFLR3.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2940
Number of elements = 12771
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7319
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2497
Number of elements = 10947
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6395
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
ok
test_setInput (test_aflr3.TestAFLR3.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr3.TestAFLR3.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5047
Number of elements = 27987
Number of triangles = 3464
Number of quadrilatarals = 0
Number of tetrahedrals = 24523
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_torus (test_aflr3.TestAFLR3.test_torus) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6342
Number of elements = 35410
Number of triangles = 4052
Number of quadrilatarals = 0
Number of tetrahedrals = 31358
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_transp (test_aflr3.TestAFLR3.test_transp) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 60311
Number of elements = 351913
Number of triangles = 12928
Number of quadrilatarals = 0
Number of tetrahedrals = 338985
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 59175
Number of elements = 344623
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 332195
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 60311
Number of elements = 351413
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 338985
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_MultiBody_quad (test_aflr4.TestAFLR4.test_MultiBody_quad) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
ok
test_SingleBody_output (test_aflr4.TestAFLR4.test_SingleBody_output) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - trailingEdge
Done getting mesh sizing parameters
ok
test_all (test_aflr4.TestAFLR4.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
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:62408)
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:62408)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
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:62408)
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:62408)
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:62408)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
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:62408)
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:62408)
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
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:62408)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ok
test_reenter (test_aflr4.TestAFLR4.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
ok
test_regions (test_aflr4.TestAFLR4.test_regions) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = cut, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: box
2: cut
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
ok
test_setInput (test_aflr4.TestAFLR4.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr4.TestAFLR4.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_structures (test_aflr4.TestAFLR4.test_structures) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = LeadingEdge, index = 1
Name = TrailingEdge, index = 2
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Ribs
2: Skin
3: Spar1
4: Rib_Root
5: Spar2
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
ok
test_torus (test_aflr4.TestAFLR4.test_torus) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_Aeroelastic (test_astros.TestAstros.test_Aeroelastic) ... skipped 'No astros.exe executable'
test_Plate (test_astros.TestAstros.test_Plate) ... skipped 'No astros.exe executable'
test_MassProp_Units (test_avl.TestAVL.test_MassProp_Units) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_MassProp_noUnits (test_avl.TestAVL.test_MassProp_noUnits) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_alpha_custom_increment (test_avl.TestAVL.test_alpha_custom_increment) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_geom_change (test_avl.TestAVL.test_geom_change) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
ok
test_numSpan (test_avl.TestAVL.test_numSpan) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
ok
test_phase (test_avl.TestAVL.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_wing_Vtail (test_avl.TestAVL.test_wing_Vtail) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - VTail1
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - VTail2
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - VTail1 (ID = 0)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - VTail2 (ID = 1)
Section 1 of 2 (ID = 0)
Section 2 of 2 (ID = 1)
Writing surface - Wing (ID = 2)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
ok
test_wing_tail (test_avl.TestAVL.test_wing_tail) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
VLM surface name - hTail
VLM surface name - vTail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing surface - hTail (ID = 1)
Section 1 of 3 (ID = 2)
Control surface 1 of 1
Section 2 of 3 (ID = 1)
Control surface 1 of 1
Section 3 of 3 (ID = 0)
Control surface 1 of 1
Writing surface - vTail (ID = 2)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
ok
test_wing_tail_control (test_avl.TestAVL.test_wing_tail_control) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice control surface data
VLM control surface name - Elevator
VLM control surface name - LeftAileron
VLM control surface name - RightAileron
VLM control surface name - Rudder
Done getting vortex lattice control surface data
Getting vortex lattice surface data
VLM surface name - Wing
VLM surface name - hTail
VLM surface name - vTail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing surface - hTail (ID = 1)
Section 1 of 3 (ID = 2)
Control surface 1 of 1
Section 2 of 3 (ID = 1)
Control surface 1 of 1
Section 3 of 3 (ID = 0)
Control surface 1 of 1
Writing surface - vTail (ID = 2)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
ok
test_TargetCL (test_cart3d.TestCart3D.test_TargetCL) ... skipped 'No flowCart executable'
test_outputs (test_cart3d.TestCart3D.test_outputs) ... skipped 'No flowCart executable'
test_reenter (test_cart3d.TestCart3D.test_reenter) ... skipped 'No flowCart executable'
test_sensitivity_AnalysisIn (test_cart3d.TestCart3D.test_sensitivity_AnalysisIn) ... skipped 'No flowCart executable'
test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... skipped 'No flowCart executable'
test_Output_v5 (test_cbaero.TestCBAERO.test_Output_v5) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing1, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Wing1, index = 1
Name = trailingEdge, index = 2
Writing FAST file ....
Finished writing FAST file
Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_Output_v6 (test_cbaero.TestCBAERO.test_Output_v6) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_inputs (test_cbaero.TestCBAERO.test_inputs) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_MultiBody (test_egadsTess.TestEGADS.test_MultiBody) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
ok
test_SingleBody_AnalysisOutVal (test_egadsTess.TestEGADS.test_SingleBody_AnalysisOutVal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
ok
test_all (test_egadsTess.TestEGADS.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
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
7F285657A740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7F285657A740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7F282F790700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7F282F790700 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
7F282EF8F700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7F282EF8F700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7F285657A740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7F285657A740 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
7F285657A740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7F285657A740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7F285657A740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7F285657A740 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
7F282F790700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7F282F790700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7F285657A740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7F285657A740 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:62408)
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:62408)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
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:62408)
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:62408)
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:62408)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
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:62408)
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:62408)
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:62408)
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:62408)
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:62408)
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: 0.17
Creating surface mesh ...
Surface mesh seconds: 0.04
Recovering boundaries...
Boundary recovery seconds: 0.2
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.08
Recovering Delaunayness...
Delaunay recovery seconds: 0.08
Refining mesh...
18827 insertions, added 13420 points, 721721 tetrahedra in queue.
6269 insertions, added 2485 points, 625204 tetrahedra in queue.
8356 insertions, added 2101 points, 168215 tetrahedra in queue.
Refinement seconds: 3.37
Smoothing vertices...
Mesh smoothing seconds: 3.04
Improving mesh...
Mesh improvement seconds: 0.07
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.02
Total running seconds: 7.07
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: 0.17
Creating surface mesh ...
Surface mesh seconds: 0.05
Recovering boundaries...
Boundary recovery seconds: 0.23
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.11
Recovering Delaunayness...
Delaunay recovery seconds: 0.1
Refining mesh...
18827 insertions, added 13420 points, 721721 tetrahedra in queue.
6269 insertions, added 2485 points, 625204 tetrahedra in queue.
8356 insertions, added 2101 points, 168215 tetrahedra in queue.
Refinement seconds: 3.38
Smoothing vertices...
Mesh smoothing seconds: 2.48
Improving mesh...
Mesh improvement seconds: 0.07
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.01
Total running seconds: 6.6
Statistics:
Input points: 14124
Input facets: 28236
Input segments: 42354
Input holes: 2
Input regions: 0
Mesh points: 33059
Mesh tetrahedra: 159851
Mesh faces: 333820
Mesh faces on exterior boundary: 28236
Mesh faces on input facets: 28236
Mesh edges on input segments: 42354
Steiner points inside domain: 18935
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM4/fun3d.nml .....
Appending namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
ok
test_cythonNMLError (test_fun3d.TestFUN3D.test_cythonNMLError) ... ok
test_cythonNMLReentrance (test_fun3d.TestFUN3D.test_cythonNMLReentrance) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml not found!
Creating namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml .....
Appending namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
ok
test_invalidBoundary (test_fun3d.TestFUN3D.test_invalidBoundary) ... Getting CFD boundary conditions
Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_fun3d.TestFUN3D.test_invalidBoundaryName) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - X
ok
test_journal (test_fun3d.TestFUN3D.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 5043, elements - 10074
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 5043, elements - 10074
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
ok
test_moving_body (test_fun3d.TestFUN3D.test_moving_body) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Writing moving_body.input
ok
test_overwriteNML (test_fun3d.TestFUN3D.test_overwriteNML) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_phase (test_fun3d.TestFUN3D.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 14124, elements - 28236
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_reenter (test_fun3d.TestFUN3D.test_reenter) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
ok
test_symmetry (test_fun3d.TestFUN3D.test_symmetry) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_box1 (test_masstran.TestMasstran.test_box1) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_box2 (test_masstran.TestMasstran.test_box2) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_box3 (test_masstran.TestMasstran.test_box3) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - box2
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
ok
test_journal (test_masstran.TestMasstran.test_journal) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
ok
test_plate (test_masstran.TestMasstran.test_plate) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_plate_point (test_masstran.TestMasstran.test_plate_point) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
ok
test_Cheby_Modes (test_mses.TestMSES_Kulfan.test_Cheby_Modes) ...
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - alowervar
Design Variable name - auppervar
Design Variable name - classvar
Design Variable name - ztailvar
Done getting CFD design variables
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_Kulfan.test_Cheby_Modes_Symmetric) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - avar
Done getting CFD design variables
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_allInputs (test_mses.TestMSES_Kulfan.test_allInputs) ... ok
test_execute (test_mses.TestMSES_Kulfan.test_execute) ... ok
test_sensitivity_AnalysisIn (test_mses.TestMSES_Kulfan.test_sensitivity_AnalysisIn) ... ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_NACA.test_Cheby_Modes_Symmetric) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
ok
test_geom_sensitivity_CL (test_mses.TestMSES_NACA.test_geom_sensitivity_CL) ...
Getting CFD design variables.......
Number of design variables - 2
Design Variable name - camber
Design Variable name - thick
Done getting CFD design variables
ok
test_journal (test_mses.TestMSES_NACA.test_journal) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
ok
test_MultiBody (test_pointwise.TestPointwise.test_MultiBody) ... skipped 'No pointwise executable'
test_SingleBody (test_pointwise.TestPointwise.test_SingleBody) ... skipped 'No pointwise executable'
test_all (test_pointwise.TestPointwise.test_all) ... skipped 'No pointwise executable'
test_box (test_pointwise.TestPointwise.test_box) ... skipped 'No pointwise executable'
test_bullet (test_pointwise.TestPointwise.test_bullet) ... skipped 'No pointwise executable'
test_cone (test_pointwise.TestPointwise.test_cone) ... skipped 'No pointwise executable'
test_cylinder (test_pointwise.TestPointwise.test_cylinder) ... skipped 'No pointwise executable'
test_executeError (test_pointwise.TestPointwise.test_executeError) ... skipped 'No pointwise executable'
test_reenter (test_pointwise.TestPointwise.test_reenter) ... skipped 'No pointwise executable'
test_sphere (test_pointwise.TestPointwise.test_sphere) ... skipped 'No pointwise executable'
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
test_Area_Mesh (test_refine.TestREFINE.test_Area_Mesh) ... skipped "No 'ref' executable"
test_all (test_refine.TestREFINE.test_all) ... skipped "No 'ref' executable"
test_box_volume (test_refine.TestREFINE.test_box_volume) ... skipped "No 'ref' executable"
test_boxhole (test_refine.TestREFINE.test_boxhole) ... skipped "No 'ref' executable"
test_cfdSingleBody (test_refine.TestREFINE.test_cfdSingleBody) ... skipped "No 'ref' executable"
test_fun3d (test_refine.TestREFINE.test_fun3d) ... skipped "No 'ref' executable"
test_inputs (test_refine.TestREFINE.test_inputs) ... skipped "No 'ref' executable"
test_phase (test_refine.TestREFINE.test_phase) ... skipped "No 'ref' executable"
test_sphere (test_refine.TestREFINE.test_sphere) ... skipped "No 'ref' executable"
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
test_inputs (test_su2.TestSU2.test_inputs) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 3 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 8 Faces
EGADS : Body 0 has 15 Edges
EGADS : Body 0 has 8 Loops
EGADS : Body 0 has 9 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 8 Faces
EGADS : Body 1 has 15 Edges
EGADS : Body 1 has 8 Loops
EGADS : Body 1 has 9 Nodes
EGADS : Body 2 is a SolidBody
EGADS : Body 2 has 1 Shells
EGADS : Body 2 has 2 Faces
EGADS : Body 2 has 6 Edges
EGADS : Body 2 has 2 Loops
EGADS : Body 2 has 2 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 1 1 2 3 4 5
EGADS : 2 Yes 0 0 1 1 1 1 3 4 6
EGADS : 3 Yes 0 0 1 1 1 1 2 4 7
EGADS : 4 Yes 0 0 1 1 1 1 2 3
EGADS : 5 Yes 0 0 1 1 1 1 6 7 8
EGADS : 6 Yes 0 0 1 1 1 2 5 7 8
EGADS : 7 Yes 0 0 1 1 1 3 5 6 8
EGADS : 8 Yes 0 0 1 1 1 5 6 7
EGADS : 9 Yes 1 0 1 0 10 10 11 12 13
EGADS : 10 Yes 1 0 1 0 10 9 11 12 14
EGADS : 11 Yes 1 0 1 0 10 9 10 12 15
EGADS : 12 Yes 1 0 1 0 10 9 10 11
EGADS : 13 Yes 1 0 1 0 10 9 14 15 16
EGADS : 14 Yes 1 0 1 0 10 10 13 15 16
EGADS : 15 Yes 1 0 1 0 10 11 13 14 16
EGADS : 16 Yes 1 0 1 0 10 13 14 15
EGADS : 17 Yes 2 0 1 NA NA 18
EGADS : 18 Yes 2 0 1 NA NA 17
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 4 -3 -2
EGADS : 2 3 7 -6 -5
EGADS : 3 6 9 -1 -8
EGADS : 4 -4 -9 -7
EGADS : 5 -10 2 11 -12
EGADS : 6 -11 5 13 -14
EGADS : 7 -13 8 10 -15
EGADS : 8 12 14 15
EGADS : 9 16 19 -18 -17
EGADS : 10 18 22 -21 -20
EGADS : 11 21 24 -16 -23
EGADS : 12 -19 -24 -22
EGADS : 13 -25 17 26 -27
EGADS : 14 -26 20 28 -29
EGADS : 15 -28 23 25 -30
EGADS : 16 27 29 30
EGADS : 17 -31 -32 33 34
EGADS : 18 -35 -34 36 32
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : 17 17
EGADS : 18 18
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes 1 4 -3 -2
EGADS : 2 Yes 3 7 -6 -5
EGADS : 3 Yes 6 9 -1 -8
EGADS : 4 Yes -4 -9 -7
EGADS : 5 Yes -10 2 11 -12
EGADS : 6 Yes -11 5 13 -14
EGADS : 7 Yes -13 8 10 -15
EGADS : 8 Yes 12 14 15
EGADS : 9 Yes 16 19 -18 -17
EGADS : 10 Yes 18 22 -21 -20
EGADS : 11 Yes 21 24 -16 -23
EGADS : 12 Yes -19 -24 -22
EGADS : 13 Yes -25 17 26 -27
EGADS : 14 Yes -26 20 28 -29
EGADS : 15 Yes -28 23 25 -30
EGADS : 16 Yes 27 29 30
EGADS : 17 Yes -31 -32 33 34
EGADS : 18 Yes -35 -34 36 32
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 5
EGADS : 3 0 Yes 3 4 1 1 2
EGADS : 4 0 Yes 2 4 1 1 4
EGADS : 5 0 Yes 3 5 1 2 6
EGADS : 6 0 Yes 5 6 1 2 3
EGADS : 7 0 Yes 4 6 1 2 4
EGADS : 8 0 Yes 5 1 1 3 7
EGADS : 9 0 Yes 6 2 1 3 4
EGADS : 10 0 Yes 1 7 1 5 7
EGADS : 11 0 Yes 3 8 1 5 6
EGADS : 12 0 Yes 7 8 1 5 8
EGADS : 13 0 Yes 5 9 1 6 7
EGADS : 14 0 Yes 8 9 1 6 8
EGADS : 15 0 Yes 9 7 1 7 8
EGADS : 16 1 Yes 10 11 1 9 11
EGADS : 17 1 Yes 10 12 1 9 13
EGADS : 18 1 Yes 12 13 1 9 10
EGADS : 19 1 Yes 11 13 1 9 12
EGADS : 20 1 Yes 12 14 1 10 14
EGADS : 21 1 Yes 14 15 1 10 11
EGADS : 22 1 Yes 13 15 1 10 12
EGADS : 23 1 Yes 14 10 1 11 15
EGADS : 24 1 Yes 15 11 1 11 12
EGADS : 25 1 Yes 10 16 1 13 15
EGADS : 26 1 Yes 12 17 1 13 14
EGADS : 27 1 Yes 16 17 1 13 16
EGADS : 28 1 Yes 14 18 1 14 15
EGADS : 29 1 Yes 17 18 1 14 16
EGADS : 30 1 Yes 18 16 1 15 16
EGADS : 31 2 DEGEN 19 19 - 17
EGADS : 32 2 Yes 20 19 NA 17 18
EGADS : 33 2 DEGEN 20 20 - 17
EGADS : 34 2 Yes 20 19 NA 17 18
EGADS : 35 2 DEGEN 19 19 - 18
EGADS : 36 2 DEGEN 20 20 - 18
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 3.77246052 0 0.00459131419
EGADS : 2 Yes 5.90487498 7.07106781 0
EGADS : 3 Yes 0 0 0
EGADS : 4 Yes 4.0824829 7.07106781 0.123425948
EGADS : 5 Yes 3.77001182 0 0
EGADS : 6 Yes 5.90282524 7.07106781 0
EGADS : 7 Yes 5.90487498 0 0
EGADS : 8 Yes 4.0824829 0 0.123425948
EGADS : 9 Yes 5.90282524 0 0
EGADS : 10 Yes 11.5089842 0 0.00183652568
EGADS : 11 Yes 12.36195 2.82842712 0
EGADS : 12 Yes 10 0 0
EGADS : 13 Yes 11.6329932 2.82842712 0.0493703791
EGADS : 14 Yes 11.5080047 0 0
EGADS : 15 Yes 12.3611301 2.82842712 0
EGADS : 16 Yes 12.36195 0 0
EGADS : 17 Yes 11.6329932 0 0.0493703791
EGADS : 18 Yes 12.3611301 0 0
EGADS : 19 Yes 0 0 80
EGADS : 20 Yes 0 0 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 160
AFLR4 : Min Bounding Box Length = 160
AFLR4 : Max Ref Bounding Box Length = 14.1421
AFLR4 : Min Ref Bounding Box Length = 0.890888
AFLR4 : Reference Length = 0.890888
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 15.6122
AFLR4 : Abs Min Surf Spacing = 0.00222722
AFLR4 : Min Surf Spacing = 0.00445444
AFLR4 : Max Surf Spacing = 0.0890888
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD
AFLR4 : 2 CAD geometry 0 STD
AFLR4 : 3 CAD geometry 0 STD
AFLR4 : 4 CAD geometry 0 STD
AFLR4 : 5 CAD geometry 0 STD
AFLR4 : 6 CAD geometry 0 STD
AFLR4 : 7 CAD geometry 0 STD
AFLR4 : 8 CAD geometry 0 STD
AFLR4 : 9 CAD geometry 0 STD
AFLR4 : 10 CAD geometry 0 STD
AFLR4 : 11 CAD geometry 0 STD
AFLR4 : 12 CAD geometry 0 STD
AFLR4 : 13 CAD geometry 0 STD
AFLR4 : 14 CAD geometry 0 STD
AFLR4 : 15 CAD geometry 0 STD
AFLR4 : 16 CAD geometry 0 STD
AFLR4 : 17 CAD geometry 0 FARFIELD
AFLR4 : 18 CAD geometry 0 FARFIELD
AFLR4 : Case has 2 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6 7 8
AFLR4 : Component 2 includes Definitions 9 10 11 12 13 14 15 16
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR43 : INPUT SURFACE MESH FROM TESS
AFLR43 : Quad Surface Faces= 0
AFLR43 : Tria Surface Faces= 12428
AFLR43 : Nodes = 6220
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR3 : ---------------------------------------
AFLR3 : AFLR3 LIBRARY
AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3 : TETRAHEDRAL GRID GENERATOR
AFLR3 : Version Number 16.32.50
AFLR3 : Version Date 10/31/23 @ 06:31PM
AFLR3 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR3 : Compile Date 03/08/24 @ 01:03AM
AFLR3 : Copyright 1994-2021, D.L. Marcum
AFLR3 : ---------------------------------------
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 6220 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid
UG3 : 2 Solid
UG3 : 3 Solid
UG3 : 4 Solid
UG3 : 5 Solid
UG3 : 6 Solid
UG3 : 7 Solid
UG3 : 8 Solid
UG3 : 9 Solid
UG3 : 10 Solid
UG3 : 11 Solid
UG3 : 12 Solid
UG3 : 13 Solid
UG3 : 14 Solid
UG3 : 15 Solid
UG3 : 16 Solid
UG3 : 17 FarField
UG3 : 18 FarField
AFLR3 : CPU Time = 0.014 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 6220 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 1246 7333
AFLR3 IG : Nodes, Elements = 2492 16261
AFLR3 IG : Nodes, Elements = 3738 25021
AFLR3 IG : Nodes, Elements = 4984 34304
AFLR3 IG : Nodes, Elements = 6227 43518
AFLR3 IG : Nodes, Elements = 6227 43440
AFLR3 IG : Nodes, Elements = 6227 43475
AFLR3 IG : Nodes, Elements = 6227 43439
AFLR3 IG : Nodes, Elements = 6220 26110
AFLR3 IG : Nodes, Elements = 6220 26133
AFLR3 IG : Nodes, Elements = 6220 21488
AFLR3 IG : Nodes, Elements = 6220 19195
AFLR3 : CPU Time = 0.195 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 6220 19195
AFLR3 GG : Nodes, Elements = 9104 28052
AFLR3 GG : Nodes, Elements = 9104 39102
AFLR3 GG : Nodes, Elements = 9104 36335
AFLR3 GG : Nodes, Elements = 9104 34880
AFLR3 GG : Nodes, Elements = 11662 42890
AFLR3 GG : Nodes, Elements = 11662 54004
AFLR3 GG : Nodes, Elements = 11662 50843
AFLR3 GG : Nodes, Elements = 11662 49925
AFLR3 GG : Nodes, Elements = 14498 58736
AFLR3 GG : Nodes, Elements = 14498 71038
AFLR3 GG : Nodes, Elements = 14498 67638
AFLR3 GG : Nodes, Elements = 14498 66762
AFLR3 GG : Nodes, Elements = 17480 75922
AFLR3 GG : Nodes, Elements = 17480 88720
AFLR3 GG : Nodes, Elements = 17480 85188
AFLR3 GG : Nodes, Elements = 17480 84349
AFLR3 GG : Nodes, Elements = 20711 94213
AFLR3 GG : Nodes, Elements = 20711 107855
AFLR3 GG : Nodes, Elements = 20711 104214
AFLR3 GG : Nodes, Elements = 20711 103375
AFLR3 GG : Nodes, Elements = 24093 113678
AFLR3 GG : Nodes, Elements = 24093 128254
AFLR3 GG : Nodes, Elements = 24093 124257
AFLR3 GG : Nodes, Elements = 24093 123406
AFLR3 GG : Nodes, Elements = 27618 134141
AFLR3 GG : Nodes, Elements = 27618 149080
AFLR3 GG : Nodes, Elements = 27618 145168
AFLR3 GG : Nodes, Elements = 27618 144374
AFLR3 GG : Nodes, Elements = 31189 155227
AFLR3 GG : Nodes, Elements = 31189 170286
AFLR3 GG : Nodes, Elements = 31189 166309
AFLR3 GG : Nodes, Elements = 31189 165453
AFLR3 GG : Nodes, Elements = 34751 176284
AFLR3 GG : Nodes, Elements = 34751 191463
AFLR3 GG : Nodes, Elements = 34751 187411
AFLR3 GG : Nodes, Elements = 34751 186588
AFLR3 GG : Nodes, Elements = 38283 197293
AFLR3 GG : Nodes, Elements = 38283 212453
AFLR3 GG : Nodes, Elements = 38283 208438
AFLR3 GG : Nodes, Elements = 38283 207716
AFLR3 GG : Nodes, Elements = 41833 218438
AFLR3 GG : Nodes, Elements = 41833 233399
AFLR3 GG : Nodes, Elements = 41833 229556
AFLR3 GG : Nodes, Elements = 41833 228802
AFLR3 GG : Nodes, Elements = 45233 239061
AFLR3 GG : Nodes, Elements = 45233 253453
AFLR3 GG : Nodes, Elements = 45233 249686
AFLR3 GG : Nodes, Elements = 45233 248980
AFLR3 GG : Nodes, Elements = 48547 258960
AFLR3 GG : Nodes, Elements = 48547 273037
AFLR3 GG : Nodes, Elements = 48547 269340
AFLR3 GG : Nodes, Elements = 48547 268660
AFLR3 GG : Nodes, Elements = 51788 278411
AFLR3 GG : Nodes, Elements = 51788 292195
AFLR3 GG : Nodes, Elements = 51788 288655
AFLR3 GG : Nodes, Elements = 51788 288020
AFLR3 GG : Nodes, Elements = 54897 297367
AFLR3 GG : Nodes, Elements = 54897 310536
AFLR3 GG : Nodes, Elements = 54897 307175
AFLR3 GG : Nodes, Elements = 54897 306599
AFLR3 GG : Nodes, Elements = 57861 315502
AFLR3 GG : Nodes, Elements = 57861 327967
AFLR3 GG : Nodes, Elements = 57861 324838
AFLR3 GG : Nodes, Elements = 57861 324290
AFLR3 GG : Nodes, Elements = 60791 333083
AFLR3 GG : Nodes, Elements = 60791 345364
AFLR3 GG : Nodes, Elements = 60791 342206
AFLR3 GG : Nodes, Elements = 60791 341750
AFLR3 GG : Nodes, Elements = 63489 349850
AFLR3 GG : Nodes, Elements = 63489 361174
AFLR3 GG : Nodes, Elements = 63489 358324
AFLR3 GG : Nodes, Elements = 63489 357881
AFLR3 GG : Nodes, Elements = 65986 365375
AFLR3 GG : Nodes, Elements = 65986 375877
AFLR3 GG : Nodes, Elements = 65986 373150
AFLR3 GG : Nodes, Elements = 65986 372801
AFLR3 GG : Nodes, Elements = 68262 379634
AFLR3 GG : Nodes, Elements = 68262 389039
AFLR3 GG : Nodes, Elements = 68262 386682
AFLR3 GG : Nodes, Elements = 68262 386428
AFLR3 GG : Nodes, Elements = 70242 392370
AFLR3 GG : Nodes, Elements = 70242 400574
AFLR3 GG : Nodes, Elements = 70242 398524
AFLR3 GG : Nodes, Elements = 70242 398290
AFLR3 GG : Nodes, Elements = 71834 403067
AFLR3 GG : Nodes, Elements = 71834 409901
AFLR3 GG : Nodes, Elements = 71834 408035
AFLR3 GG : Nodes, Elements = 71834 407840
AFLR3 GG : Nodes, Elements = 73096 411631
AFLR3 GG : Nodes, Elements = 73096 416942
AFLR3 GG : Nodes, Elements = 73096 415543
AFLR3 GG : Nodes, Elements = 73096 415387
AFLR3 GG : Nodes, Elements = 74042 418225
AFLR3 GG : Nodes, Elements = 74042 422196
AFLR3 GG : Nodes, Elements = 74042 421120
AFLR3 GG : Nodes, Elements = 74042 421030
AFLR3 GG : Nodes, Elements = 74697 422995
AFLR3 GG : Nodes, Elements = 74697 425691
AFLR3 GG : Nodes, Elements = 74697 424979
AFLR3 GG : Nodes, Elements = 74697 424921
AFLR3 GG : Nodes, Elements = 75147 426271
AFLR3 GG : Nodes, Elements = 75147 428179
AFLR3 GG : Nodes, Elements = 75147 427658
AFLR3 GG : Nodes, Elements = 75147 427613
AFLR3 GG : Nodes, Elements = 75442 428499
AFLR3 GG : Nodes, Elements = 75442 429739
AFLR3 GG : Nodes, Elements = 75442 429380
AFLR3 GG : Nodes, Elements = 75442 429354
AFLR3 GG : Nodes, Elements = 75634 429930
AFLR3 GG : Nodes, Elements = 75634 430753
AFLR3 GG : Nodes, Elements = 75634 430521
AFLR3 GG : Nodes, Elements = 75634 430497
AFLR3 GG : Nodes, Elements = 75743 430824
AFLR3 GG : Nodes, Elements = 75743 431284
AFLR3 GG : Nodes, Elements = 75743 431147
AFLR3 GG : Nodes, Elements = 75743 431140
AFLR3 GG : Nodes, Elements = 75813 431351
AFLR3 GG : Nodes, Elements = 75813 431632
AFLR3 GG : Nodes, Elements = 75813 431554
AFLR3 GG : Nodes, Elements = 75813 431549
AFLR3 GG : Nodes, Elements = 75854 431672
AFLR3 GG : Nodes, Elements = 75854 431830
AFLR3 GG : Nodes, Elements = 75854 431793
AFLR3 GG : Nodes, Elements = 75854 431785
AFLR3 GG : Nodes, Elements = 75878 431857
AFLR3 GG : Nodes, Elements = 75878 431960
AFLR3 GG : Nodes, Elements = 75878 431923
AFLR3 GG : Nodes, Elements = 75878 431919
AFLR3 GG : Nodes, Elements = 75896 431973
AFLR3 GG : Nodes, Elements = 75896 432050
AFLR3 GG : Nodes, Elements = 75896 432029
AFLR3 GG : Nodes, Elements = 75896 432027
AFLR3 GG : Nodes, Elements = 75911 432072
AFLR3 GG : Nodes, Elements = 75911 432140
AFLR3 GG : Nodes, Elements = 75911 432115
AFLR3 GG : Nodes, Elements = 75911 432113
AFLR3 GG : Nodes, Elements = 75917 432131
AFLR3 GG : Nodes, Elements = 75917 432161
AFLR3 GG : Nodes, Elements = 75917 432148
AFLR3 GG : Nodes, Elements = 75917 432146
AFLR3 GG : Nodes, Elements = 75922 432161
AFLR3 GG : Nodes, Elements = 75922 432186
AFLR3 GG : Nodes, Elements = 75922 432175
AFLR3 GG : Nodes, Elements = 75925 432184
AFLR3 GG : Nodes, Elements = 75925 432192
AFLR3 GG : Nodes, Elements = 75925 432191
AFLR3 GG : Nodes, Elements = 75927 432197
AFLR3 GG : Nodes, Elements = 75927 432207
AFLR3 GG : Nodes, Elements = 75927 432204
AFLR3 GG : Nodes, Elements = 75929 432210
AFLR3 GG : Nodes, Elements = 75929 432216
AFLR3 GG : Nodes, Elements = 75929 432215
AFLR3 GG : Nodes, Elements = 75932 432224
AFLR3 GG : Nodes, Elements = 75932 432240
AFLR3 GG : Nodes, Elements = 75932 432234
AFLR3 GG : Nodes, Elements = 75932 432233
AFLR3 GG : Nodes, Elements = 75933 432236
AFLR3 GG : Nodes, Elements = 75933 432244
AFLR3 GG : Nodes, Elements = 75933 432241
AFLR3 GG : Nodes, Elements = 75933 432240
AFLR3 GG : Nodes, Elements = 75962 432327
AFLR3 GG : Nodes, Elements = 75962 432440
AFLR3 GG : Nodes, Elements = 75962 432401
AFLR3 GG : Nodes, Elements = 75962 432400
AFLR3 GG : Nodes, Elements = 75964 432406
AFLR3 GG : Nodes, Elements = 75964 432411
AFLR3 GG : Nodes, Elements = 75964 432408
AFLR3 : CPU Time = 7.203 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 75964 432408
AFLR3 QI : Nodes, Elements = 74464 423905
AFLR3 QI : Nodes, Elements = 74236 422620
AFLR3 QI : Nodes, Elements = 74218 422515
AFLR3 QI : Nodes, Elements = 74218 426676
AFLR3 QI : Nodes, Elements = 74218 422354
AFLR3 QI : Nodes, Elements = 74218 421937
AFLR3 QI : Nodes, Elements = 74218 422317
AFLR3 QI : Nodes, Elements = 74218 421673
AFLR3 QI : Nodes, Elements = 74218 421449
AFLR3 QI : Nodes, Elements = 74218 421720
AFLR3 QI : Nodes, Elements = 74218 421413
AFLR3 QI : Nodes, Elements = 74218 421313
AFLR3 QI : Nodes, Elements = 74218 421535
AFLR3 QI : Nodes, Elements = 74218 421304
AFLR3 QI : Nodes, Elements = 74218 421266
AFLR3 QI : Nodes, Elements = 74218 421471
AFLR3 QI : Nodes, Elements = 74218 421263
AFLR3 QI : Nodes, Elements = 74218 421232
AFLR3 QI : Nodes, Elements = 74223 421255
AFLR3 QI : Nodes, Elements = 74223 421470
AFLR3 QI : Nodes, Elements = 74223 421272
AFLR3 QI : Nodes, Elements = 74223 421260
AFLR3 QI : Nodes, Elements = 74223 421451
AFLR3 QI : Nodes, Elements = 74223 421266
AFLR3 QI : Nodes, Elements = 74223 421234
AFLR3 : CPU Time = 2.009 seconds
AFLR3 QRG: QUALITY GRID RE-GENERATION
AFLR3 QRG: Nodes, Elements = 74223 421234
AFLR3 QRG: Nodes, Elements = 74223 421233
AFLR3 QRG: Nodes, Elements = 74223 421232
AFLR3 QRG: Nodes, Elements = 74225 421243
AFLR3 QRG: Nodes, Elements = 74230 421269
AFLR3 QRG: Nodes, Elements = 74239 421316
AFLR3 : CPU Time = 0.113 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 421316
UG3 : Min, Max Ang = 1.064 171.4
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 62
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 2.12e+06
UG3 : No. Tet Elems = 421316
UG3 : Min Vol = 6.77e-10
UG3 : Average Vol = 5.04
UG3 : Total-Tet-Vol = 2.12e+06
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : No. Tet Elems = 421316
UG3 : Min, Max Q = 0.0787 1
UG3 : Average Q = 0.894
UG3 : No. Q< 0.1 = 24
UG3 : No. Q< 0.01 = 0
OVERALL : CPU Time = 9.913 seconds
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 421316
UG3 : Min, Max Ang = 1.064 171.4
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 62
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 2.12e+06
UG3 : No. Tet Elems = 421316
UG3 : Min Vol = 6.77e-10
UG3 : Average Vol = 5.04
UG3 : Total-Tet-Vol = 2.12e+06
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : Note that L includes scaling for BL-aspect=ratio
UG3 : No. Tet Elems = 421316
UG3 : Min, Max Q = 0.188 1
UG3 : Average Q = 0.854
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : CPU Time = 0.000 seconds
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : CREATE EGADS TESS FROM AFLR3 DATA
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 15
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 8
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 16
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 17
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 18
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 30
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 9
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 10
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 16
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 32
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 34
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 17
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 18
EGADS : EGADS TESS CREATED
EGADS : CHECK TESS FACE NODE MAP
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 9
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 10
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 16
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 17
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 18
Volume mesh:
Number of nodes = 74239
Number of elements = 433744
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 421316
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Cardinal"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Raven"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Falcon"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
ok
test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ... Getting CFD boundary conditions
Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - X
ok
test_journal (test_su2.TestSU2.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 74239
Number of elements = 433744
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 421316
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 1
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 2
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 74239
Number of elements = 433744
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 421316
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
CAPS Info: Hit last success -- going live!
Running SU2 1
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
CAPS Info: Hit last success -- going live!
Running SU2 2
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
ok
test_phase (test_su2.TestSU2.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 74239
Number of elements = 433744
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 421316
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_reenter (test_su2.TestSU2.test_reenter) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
ok
test_units (test_su2.TestSU2.test_units) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_PlateSensFile (test_tacs.TestTACS.test_PlateSensFile) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Projecting tessellation 1 (of 1) on to new body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Projecting tessellation 1 (of 1) on to new body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
ok
test_Multiple_Mesh (test_tetgen.TestTETGEN.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
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)
7F282E78E700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7F282E78E700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7F285657A740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7F285657A740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Getting surface mesh for body 7 (of 7)
Body 1 (of 7)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 2 (of 7)
Number of nodes = 296
Number of elements = 588
Number of triangle elements = 588
Number of quadrilateral elements = 0
Body 3 (of 7)
Number of nodes = 487
Number of elements = 970
Number of triangle elements = 970
Number of quadrilateral elements = 0
Body 4 (of 7)
Number of nodes = 2048
Number of elements = 4096
Number of triangle elements = 4096
Number of quadrilateral elements = 0
Body 5 (of 7)
Number of nodes = 152
Number of elements = 300
Number of triangle elements = 300
Number of quadrilateral elements = 0
Body 6 (of 7)
Number of nodes = 624
Number of elements = 1248
Number of triangle elements = 1248
Number of quadrilateral elements = 0
Body 7 (of 7)
Number of nodes = 488
Number of elements = 972
Number of triangle elements = 972
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 4193
Total number of elements = 8366
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 296, elements - 588
Body 3 number of surface: nodes - 487, elements - 970
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cylinder, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cone, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = torus, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = sphere, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = boxhole, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = bullet, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 296, elements - 588
Body 3 number of surface: nodes - 487, elements - 970
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Number of surface: nodes - 4193, elements - 8366
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_faceMatch_MultiDomain (test_tetgen.TestTETGEN.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 374
Number of elements = 744
Number of triangle elements = 744
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 472
Total number of elements = 936
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 386
Number of elements = 768
Number of triangle elements = 768
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 582
Total number of elements = 1152
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 351
Number of elements = 698
Number of triangle elements = 698
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 491
Total number of elements = 970
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 376
Number of elements = 748
Number of triangle elements = 748
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 516
Total number of elements = 1020
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 370
Number of elements = 736
Number of triangle elements = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 454
Total number of elements = 896
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 370
Number of elements = 736
Number of triangle elements = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 126
Number of elements = 252
Number of triangle elements = 252
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 20
Number of elements = 36
Number of triangle elements = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 516
Total number of elements = 1024
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 109
Number of elements = 214
Number of triangle elements = 214
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 48
Number of elements = 96
Number of triangle elements = 96
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 12
Number of elements = 20
Number of triangle elements = 20
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 169
Total number of elements = 330
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 536
Number of elements = 1072
Number of triangle elements = 1072
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 544
Number of elements = 1084
Number of triangle elements = 1084
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1080
Total number of elements = 2156
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 5)
Getting surface mesh for body 2 (of 5)
Getting surface mesh for body 3 (of 5)
Getting surface mesh for body 4 (of 5)
Getting surface mesh for body 5 (of 5)
Body 1 (of 5)
Number of nodes = 1352
Number of elements = 2684
Number of triangle elements = 2684
Number of quadrilateral elements = 0
Body 2 (of 5)
Number of nodes = 288
Number of elements = 572
Number of triangle elements = 572
Number of quadrilateral elements = 0
Body 3 (of 5)
Number of nodes = 173
Number of elements = 342
Number of triangle elements = 342
Number of quadrilateral elements = 0
Body 4 (of 5)
Number of nodes = 26
Number of elements = 48
Number of triangle elements = 48
Number of quadrilateral elements = 0
Body 5 (of 5)
Number of nodes = 482
Number of elements = 960
Number of triangle elements = 960
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 2321
Total number of elements = 4606
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1352, elements - 2684
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 173, elements - 342
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1352, elements - 2684
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 173, elements - 342
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 440
Number of elements = 876
Number of triangle elements = 876
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 522
Number of elements = 1044
Number of triangle elements = 1044
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 962
Total number of elements = 1920
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 440, elements - 876
Body 2 number of surface: nodes - 522, elements - 1044
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 440, elements - 876
Body 2 number of surface: nodes - 522, elements - 1044
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_journal (test_tetgen.TestTETGEN.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
ok
test_phase (test_tetgen.TestTETGEN.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 7130, elements - 14252
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_reenter (test_tetgen.TestTETGEN.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 9626
Number of elements = 19244
Number of triangle elements = 19244
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9626
Total number of elements = 19244
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
ok
test_setInput (test_tetgen.TestTETGEN.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_Cl (test_xfoil.Testxfoil_Kulfan.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_Kulfan.test_alpha_custom_increment) ... ok
test_CL_uniform_increment (test_xfoil.Testxfoil_NACA.test_CL_uniform_increment) ... ok
test_Cl (test_xfoil.Testxfoil_NACA.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_NACA.test_alpha_custom_increment) ... ok
test_alpha_uniform_inrement (test_xfoil.Testxfoil_NACA.test_alpha_uniform_inrement) ... ok
test_append (test_xfoil.Testxfoil_NACA.test_append) ... ok
test_normalize (test_xfoil.Testxfoil_NACA.test_normalize) ... ok
test_phase (test_xfoil.Testxfoil_NACA.test_phase) ... ok
test_Output (test_zaero.TestZAERO.test_Output) ... ok
test_inputs (test_zaero.TestZAERO.test_inputs) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Rib_Root_Point, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = LeadingEdge, index = 1
Name = TrailingEdge, index = 2
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1220
Number of elements = 2680
Number of triangle elements = 2680
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1221
Total number of elements = 2680
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Rib_Root, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Rib_Root_Point, index = 6
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1220
Number of elements = 2680
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 2680
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 1221
Combined Number of elements = 2681
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 2680
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 1
Material name - madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 6
Property name - Rib_Root
Property name - Rib_Root_Point
Property name - Ribs
Property name - Skin
Property name - Spar1
Property name - Spar2
Done getting FEA properties
Updating mesh element types based on properties input
'Smart_Restart' is ON
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting vortex lattice control surface data
VLM control surface name - CntrlLE
VLM control surface name - CntrlTE
Done getting vortex lattice control surface data
Getting FEA vortex lattice mesh
Getting ZAERO UAIC Configurations.......
Number of UAIC Configurations - 2
UAIC Configuration: climb, id = 1
- Mach Number : 0.200000
- Reduced Freq: [0.020000, ... , 0.250000]
UAIC Configuration: cruise, id = 2
- Mach Number : 0.700000
- Reduced Freq: [0.040000, ... , 0.350000]
Getting ZAERO Analysis Subcases.......
Number of Analysis Subcases - 2
Analysis Subcase: FlutterCruise, id = 1
- Discipline : flutter
- UAIC : cruise
Analysis Subcase: Trim, id = 2
- Discipline : Trim
- UAIC : climb
Getting ZAERO Trim Variables.......
Number of Trim Variables - 2
Trim Variable: ANGLEA
- Label : ALPHA
- Value : free
Trim Variable: URDD3
- Label : NZ
- Value : 1.0
Updating StaticAeroelastic subcase: Trim
- vectorToCG -> [0.345898, 1.652951, -0.041403]
- weight -> 476456.149985
- weightMomentOfInertia -> [304902.643270, 98963.803820, 69822.813292, 6179.981375, 19723.152207, 370546.335524]
ok
----------------------------------------------------------------------
Ran 146 tests in 549.636s
OK (skipped=26)
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/
+ make test TYPE=MINIMAL
(make -C cCAPS -f aeroelastic_SU2.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `avlTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `awaveTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `frictionTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: Nothing to be done for `fun3d'.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f hsm.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `hsm' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `interferenceTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `msesTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f mystran.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `mystranTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `pointwiseTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(cd ./regressionTest; ./execute_CTestRegression.sh MINIMAL)
Running.... MINIMAL c-Tests
All tests pass!
(cd ./regressionTest; ./execute_PyTestRegression.sh MINIMAL)
=================================================
Using python : /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python
=================================================
Running.... MINIMAL PyTests
=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
CXtot 0.0006119078685746836
CYtot -6.288067668554914e-15
CZtot -0.3012861394886091
Cltot -4.782099331324466e-14
Cmtot -0.1945055953450467
Cntot -2.339543963831951e-15
Cl'tot -4.785454061647156e-14
Cn'tot -1.504596228417061e-15
CLtot 0.3012509314150772
CDtot 0.004646353488232841
CDvis 0.0
CLff 0.3009503023520527
CYff -7.718708857566269e-15
CDind 0.004646353488232841
CDff 0.004968969500908292
e 0.9669902146157957
StripForces
Wing cl = [0.02994790451347, 0.08555545178934, 0.1329003532588, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.310122128419, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805665, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996428, 0.2453427152623, 0.2100182422922, 0.1733025192801, 0.1329003532723, 0.08555545180788, 0.0299479045408]
Wing cd = [-0.004234137763162, -0.004494543653191, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946402, 0.0005114598078397, 0.0021191472861, 0.004145189908974, 0.006609094404182, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.00660909440444, 0.004145189909261, 0.002119147286385, 0.0005114598080999, -0.000738653894407, -0.001762021024095, -0.002739626801367, -0.003752887372445, -0.004494543653161, -0.004234137764545]
real 0m0.635s
user 0m0.447s
sys 0m0.302s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
Cl = [1.05475230552567, 1.36488869373635, 1.56607214272105, 2.03059709344862, 1.97271083121169, 1.87307153172386, 1.76050475760117]
Cd = [0.0131991208675727, 0.0166540240605751, 0.0200551482562831, 0.0458671341969345, 0.0754256009394856, 0.0994469174477522, 0.127479430989037]
Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0]
Transition location = [0.4960441144043, 0.461377732041502, 0.44237656820185, 0.361251636355465, 0.276104140853559, 0.214381239321467, 0.132988264746661]
real 0m5.068s
user 0m4.927s
sys 0m0.297s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'mses_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl = 0.37837910855492407
Cd = 0.007775858417210143
Cm = 0.005262636995811319
real 0m5.000s
user 0m4.808s
sys 0m0.319s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'friction_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting Mach & Altitude Values
Lifting Surface: Body = 1, units m
XLE: 1.571946 -3.872983 0.249728
XTE: 2.536563 -3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 2, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.614012 0.000000 0.002015
Chord: 1.614013
Arc: 3.308635
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 3, units m
XLE: 1.571946 3.872983 0.249728
XTE: 2.536563 3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 4, units m
XLE: 5.484123 0.000000 1.468246
XTE: 6.210307 0.000915 1.468246
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 5, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.210307 0.001525 0.500000
Chord: 1.210308
Arc: 2.471195
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 6, units m
XLE: 5.484123 -0.968246 0.500000
XTE: 6.210307 -0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 7, units m
XLE: 5.484123 0.968246 0.500000
XTE: 6.210307 0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 8, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 9, units m
Arc: 3.714180
Diameter: 1.020621
Type: Fuse
Body of Revolution: Body = 10, units m
Arc: 2.771209
Diameter: 0.645497
Type: Fuse
Body of Revolution: Body = 11, units m
Arc: 1.013945
Diameter: 0.322749
Type: Fuse
Body of Revolution: Body = 12, units m
Arc: 0.101394
Diameter: 0.032275
Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2
Total drag = [0.0132, 0.01226]
Form drag = [0.0033, 0.00307]
Friction drag = [0.0099, 0.00919]
real 0m0.497s
user 0m0.360s
sys 0m0.203s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'tsfoil_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tsfoil_PyTest.py test;
+ python -u tsfoil_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Getting results
PAUSE Press the ENTER key to exit
To resume execution, type go. Other input will terminate the job.
Cl = 0.933329
Cd = 0.000283
Cd Wave = 0.0
Cm = -0.203433
Cp _Critcal = -1.303869
real 0m0.557s
user 0m0.386s
sys 0m0.233s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'delaundo_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Name = AirfoilTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 6
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Name = AirfoilTE, index = 6
Getting mesh sizing parameters
Mesh sizing name - Airfoil
Mesh sizing name - AirfoilTE
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting edge discretization for body 1
Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping!
Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
Writing out *.pts file
Reading delaundo mesh file - delaundo_CAPS.mesh
Swapping y and z coordinates!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
real 0m0.651s
user 0m0.488s
sys 0m0.224s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case delaundo_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'egadsTess_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Rib_Root_Point, index = 6
Name = Wing, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = LeadingEdge, index = 1
Name = TrailingEdge, index = 2
Getting mesh sizing parameters
Mesh sizing name - LeadingEdge
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 4)
Getting surface mesh for body 2 (of 4)
Getting surface mesh for body 3 (of 4)
Getting surface mesh for body 4 (of 4)
Body 1 (of 4)
Number of nodes = 3793
Number of elements = 4001
Number of triangle elements = 0
Number of quadrilateral elements = 4001
Body 2 (of 4)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes = 76
Number of elements = 55
Number of triangle elements = 0
Number of quadrilateral elements = 55
Body 4 (of 4)
Number of nodes = 100
Number of elements = 73
Number of triangle elements = 0
Number of quadrilateral elements = 73
----------------------------
Total number of nodes = 3970
Total number of elements = 4129
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
real 0m8.767s
user 0m12.867s
sys 0m0.665s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case egadsTess_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr2_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 04/23/24 @ 12:17PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 316 634
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.001 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 344 344
AFLR2 GGp: Nodes, Faces = 681 1018
AFLR2 GGp: Nodes, Faces = 1013 1682
AFLR2 GGp: Nodes, Faces = 1339 2334
AFLR2 GGp: Nodes, Faces = 1652 2960
AFLR2 GGp: Nodes, Faces = 1957 3570
AFLR2 GGp: Nodes, Faces = 2252 4160
AFLR2 GGp: Nodes, Faces = 2526 4708
AFLR2 GGp: Nodes, Faces = 2809 5274
AFLR2 GGp: Nodes, Faces = 3083 5822
AFLR2 GGp: Nodes, Faces = 3327 6310
AFLR2 GGp: Nodes, Faces = 3564 6784
AFLR2 GGp: Nodes, Faces = 3788 7232
AFLR2 GGp: Nodes, Faces = 3995 7646
AFLR2 GGp: Nodes, Faces = 4194 8044
AFLR2 GGp: Nodes, Faces = 4394 8444
AFLR2 GGp: Nodes, Faces = 4585 8826
AFLR2 GGp: Nodes, Faces = 4772 9200
AFLR2 GGp: Nodes, Faces = 4943 9542
AFLR2 GGp: Nodes, Faces = 5129 9914
AFLR2 GGp: Nodes, Faces = 5293 10242
AFLR2 GGp: Nodes, Faces = 5447 10550
AFLR2 GGp: Nodes, Faces = 5594 10844
AFLR2 GGp: Nodes, Faces = 5716 11088
AFLR2 GGp: Nodes, Faces = 5830 11316
AFLR2 GGp: Nodes, Faces = 5909 11474
AFLR2 GGp: Nodes, Faces = 5964 11584
AFLR2 GGp: Nodes, Faces = 6006 11668
AFLR2 GGp: Nodes, Faces = 6025 11706
AFLR2 GGp: Nodes, Faces = 6034 11724
AFLR2 : CPU Time = 0.026 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 = 0.013 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 0m0.774s
user 0m0.700s
sys 0m0.334s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr4_and_aflr3_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_aflr3_PyTest.py test;
+ python -u aflr4_and_aflr3_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Wing1
Mesh sizing name - Wing2
Done getting mesh sizing parameters
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 04/23/24 @ 12:17PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR4 : Compile Date 04/23/24 @ 12:17PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 151604
Number of elements = 458324
Number of triangles = 14380
Number of quadrilatarals = 0
Number of tetrahedrals = 222892
Number of pyramids = 425
Number of prisms = 220627
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
real 0m16.332s
user 0m16.050s
sys 0m0.421s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'tetgen_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 2236
Number of elements = 4468
Number of triangle elements = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 636
Number of elements = 1268
Number of triangle elements = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 267
Number of elements = 530
Number of triangle elements = 530
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 3139
Total number of elements = 6266
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 3139, elements - 6266
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.03
Creating surface mesh ...
Surface mesh seconds: 0
Recovering boundaries...
Boundary recovery seconds: 0.06
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.01
Suppressing Steiner points ...
Steiner suppression seconds: 0
Recovering Delaunayness...
Delaunay recovery seconds: 0.01
Refining mesh...
4190 insertions, added 2180 points, 134280 tetrahedra in queue.
1395 insertions, added 459 points, 138994 tetrahedra in queue.
1859 insertions, added 487 points, 137112 tetrahedra in queue.
2478 insertions, added 498 points, 120303 tetrahedra in queue.
3304 insertions, added 499 points, 74342 tetrahedra in queue.
4404 insertions, added 474 points, 460 tetrahedra in queue.
Refinement seconds: 0.73
Smoothing vertices...
Mesh smoothing seconds: 0.53
Improving mesh...
Mesh improvement seconds: 0.02
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0
Total running seconds: 1.39
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 0m2.795s
user 0m2.870s
sys 0m0.285s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tetgen_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_and_AFLR2_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_PyTest.py test;
+ python -u su2_and_AFLR2_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Saving geometry
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 04/23/24 @ 12:17PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 545 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 545 545
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 110 222
AFLR2 IG : Nodes, Faces = 220 442
AFLR2 IG : Nodes, Faces = 330 662
AFLR2 IG : Nodes, Faces = 440 882
AFLR2 IG : Nodes, Faces = 517 1036
AFLR2 IG : Nodes, Faces = 545 1092
AFLR2 IG : Nodes, Faces = 549 1092
AFLR2 IG : Nodes, Faces = 545 545
AFLR2 : CPU Time = 0.002 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 545 545
AFLR2 GGp: Nodes, Faces = 1083 1621
AFLR2 GGp: Nodes, Faces = 1616 2687
AFLR2 GGp: Nodes, Faces = 2144 3743
AFLR2 GGp: Nodes, Faces = 2661 4777
AFLR2 GGp: Nodes, Faces = 3171 5797
AFLR2 GGp: Nodes, Faces = 3672 6799
AFLR2 GGp: Nodes, Faces = 4158 7771
AFLR2 GGp: Nodes, Faces = 4653 8761
AFLR2 GGp: Nodes, Faces = 5142 9739
AFLR2 GGp: Nodes, Faces = 5608 10671
AFLR2 GGp: Nodes, Faces = 6055 11565
AFLR2 GGp: Nodes, Faces = 6482 12419
AFLR2 GGp: Nodes, Faces = 6880 13215
AFLR2 GGp: Nodes, Faces = 7257 13969
AFLR2 GGp: Nodes, Faces = 7614 14683
AFLR2 GGp: Nodes, Faces = 7947 15349
AFLR2 GGp: Nodes, Faces = 8276 16007
AFLR2 GGp: Nodes, Faces = 8575 16605
AFLR2 GGp: Nodes, Faces = 8869 17193
AFLR2 GGp: Nodes, Faces = 9140 17735
AFLR2 GGp: Nodes, Faces = 9401 18257
AFLR2 GGp: Nodes, Faces = 9654 18763
AFLR2 GGp: Nodes, Faces = 9887 19229
AFLR2 GGp: Nodes, Faces = 10110 19675
AFLR2 GGp: Nodes, Faces = 10315 20085
AFLR2 GGp: Nodes, Faces = 10497 20449
AFLR2 GGp: Nodes, Faces = 10656 20767
AFLR2 GGp: Nodes, Faces = 10791 21037
AFLR2 GGp: Nodes, Faces = 10919 21293
AFLR2 GGp: Nodes, Faces = 11022 21499
AFLR2 GGp: Nodes, Faces = 11092 21639
AFLR2 GGp: Nodes, Faces = 11145 21745
AFLR2 GGp: Nodes, Faces = 11156 21767
AFLR2 : CPU Time = 0.046 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 = 0.017 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| 1.0306e-01| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.0096e-01| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 9.9106e-02| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 9.8049e-02| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 9.7401e-02| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 9.7044e-02| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 9.6376e-02| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 9.5925e-02| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 9.5703e-02| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 9.5462e-02| -1.221243| 1.499646| 1.130319| 4.189559| -6.277653|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.22124| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_pyCAPS_su2_aflr2.dat |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|CSV file |surface_flow_pyCAPS_su2_aflr2.csv |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary |flow_pyCAPS_su2_aflr2.szplt |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary surface |surface_flow_pyCAPS_su2_aflr2.szplt|
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 994 more values.0: Error finishing Tecplot file output.
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
+-----------------------------------------------------------------------+
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.072253 Cd = -0.01151
Cmz = 0.070975
Cx = -0.01151 Cy = 0.072253
Pressure Contribution
Cl_p = 0.072253 Cd_p = -0.01151
Cmz_p = 0.070975
Cx_p = -0.01151 Cy_p = 0.072253
Viscous Contribution
Cl_v = 0.0 Cd_v = 0.0
Cmz_v = 0.0
Cx_v = 0.0 Cy_v = 0.0
real 0m2.204s
user 0m1.974s
sys 0m0.393s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'masstran_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Getting results mass properties.....
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 1159
Number of elements = 798
Number of triangle elements = 0
Number of quadrilateral elements = 798
----------------------------
Total number of nodes = 1159
Total number of elements = 798
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1159
Number of elements = 798
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 798
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - Ribs_and_Spars
No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Area 3.428666259747
Mass 5383.006027803
Centroid [1.222256036874, 0.1634981473778, -4.234505810751e-11]
CG [1.222256036874, 0.1634981473778, -4.234637807833e-11]
Ixx 22133.97306033
Iyy 23448.30046709
Izz 1389.213122582
Ixy 164.2055275657
Ixz -7.45484669011e-06
Iyz 1.707686795832e-06
I [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.45484669011e-06, 1.707686795832e-06]
II [[22133.97306033, -164.2055275657, 7.45484669011e-06], [-164.2055275657, 23448.30046709, -1.707686795832e-06], [7.45484669011e-06, -1.707686795832e-06, 1389.213122582]]
real 0m4.564s
user 0m6.121s
sys 0m0.953s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=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 = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 81
Number of elements = 96
Elemental Tria3 = 0
Elemental Quad4 = 64
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 9
MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 32
->HSMSOL
Matrix Non-zero Entries = 5741
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.130E-01 0.165E+00 0.153E-04 1.000 ddy @ ( 0.25 0.06 0.00)
1* 0.260E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
1* 0.240E-05 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.09 0.00)
2 0.379E-02 0.505E-01 0.750E-04 1.000 ddy @ ( 0.25 0.19 0.00)
2* 0.420E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
3 0.168E-02 0.225E-01 0.208E-04 1.000 ddy @ ( 0.25 0.06 0.00)
4 0.325E-03 0.427E-02 0.250E-05 1.000 ddy @ ( 0.25 0.19 0.00)
5 0.794E-05 0.112E-03 0.170E-06 1.000 ddy @ ( 0.25 0.19 0.00)
6 0.387E-08 0.598E-07 0.197E-09 1.000 ddy @ ( 0.25 0.06 0.00)
7 0.848E-15 0.147E-13 0.924E-15 1.000 ddy @ ( 0.25 0.19 0.00)
Converging n vectors ...
it = 1 dn = 0.788E-01 rlx = 1.000 ( 59 )
it = 2 dn = 0.566E-16 rlx = 1.000 ( 35 )
Converging e1,e2 vectors ...
it = 1 de = 0.691E-03 rlx = 1.000 ( 45 )
it = 2 de = 0.404E-04 rlx = 1.000 ( 9 )
it = 3 de = 0.142E-07 rlx = 1.000 ( 46 )
it = 4 de = 0.521E-11 rlx = 1.000 ( 62 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat
real 0m1.356s
user 0m1.232s
sys 0m0.205s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ echo '../corsairlite/qp.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
../corsairlite/qp.py test;
+ python -u ../corsairlite/qp.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Objective
---------
-21.56250 dimensionless
Variables
---------
x : 1.62500 [-] The X variable
y : 1.37500 [-] The Y variable
Constants
---------
c : 3 [-] A constant
c2 : 2 [-] A constant
Sensitivities
-------------
c : + 0.46957 A constant
c2 : - 0.22338 A constant
Solve Report
------------
Solve Method : Quadratic Program
Classification : Convex
Solver : cvxopt
real 0m2.502s
user 0m2.503s
sys 0m0.531s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case ../corsairlite/qp.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Did not run examples for:
abaqus
awave
Cart3D
Astros
Mystran
=================================================
All tests pass!
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64
+ mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/test/plugs
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/test/plugs
+ sort -f
+ find /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/Plugs -name 'plugs0*.csm'
find: ‘/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/Plugs’: No such file or directory
+ awk '{ n=split($0, a, ";"); for(i=1; i<=n; i+=2) print a[i] }' /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/data/plugs/plugsFailure.txt
+ cp /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/data/plugs/plugsIgnore.txt .
+ set +x
Testing CSM files:
total 28M
-rw-rw-r--. 1 jenkins jenkins 1.3M Jun 18 21:21 ASTRO.D01
-rw-rw-r--. 1 jenkins jenkins 316K Jun 18 21:21 ASTRO.IDX
-rwxrwxr-x. 1 jenkins jenkins 1.1M Jun 18 21:21 avl
-rwxrwxr-x. 1 jenkins jenkins 29K Jun 18 21:19 egads2cart
-rwxrwxr-x. 1 jenkins jenkins 114K Jun 18 21:21 egads2cgt
-rwxrwxr-x. 1 jenkins jenkins 46K Jun 18 21:21 friction
-rwxrwxr-x. 1 jenkins jenkins 8.2M Jun 18 21:21 mastros.exe
-rwxrwxr-x. 1 jenkins jenkins 727K Jun 18 21:21 mses
-rwxrwxr-x. 1 jenkins jenkins 536K Jun 18 21:21 mset
-rwxrwxr-x. 1 jenkins jenkins 39K Jun 18 21:21 phaseUtil
-rw-rw-r--. 1 jenkins jenkins 1.6K Jun 18 21:23 pod.egads
-rw-rw-r--. 1 jenkins jenkins 0 Jun 18 21:23 port7681.jrnl
-rwxrwxr-x. 1 jenkins jenkins 451K Jun 18 21:21 pplot
-rwxrwxr-x. 1 jenkins jenkins 405K Jun 18 21:21 pxplot
-rwxrwxr-x. 1 jenkins jenkins 115K Jun 18 21:20 sensCSM
-rwxrwxr-x. 1 jenkins jenkins 507K Jun 18 21:20 serveCSM
-rwxrwxr-x. 1 jenkins jenkins 449K Jun 18 21:20 serveESP
-rwxrwxr-x. 1 jenkins jenkins 568K Jun 18 21:21 Slugs
-rwxrwxr-x. 1 jenkins jenkins 169K Jun 18 21:21 TestFit
-rwxrwxr-x. 1 jenkins jenkins 62K Jun 18 21:19 vCurvature
-rwxrwxr-x. 1 jenkins jenkins 36K Jun 18 21:19 vGeom
-rwxrwxr-x. 1 jenkins jenkins 63K Jun 18 21:19 vTess
-rwxrwxr-x. 1 jenkins jenkins 12M Jun 18 21:19 vTesstatic
-rw-rw-r--. 1 jenkins jenkins 195K Jun 18 21:23 wingMultiModel.bdf
-rwxrwxr-x. 1 jenkins jenkins 1.1M Jun 18 21:21 xfoil
[Execution node] check if [reynolds-centOS7] is in [[viggen]]
Run condition [Execution node ] preventing perform for step [Execute shell]
[Execution node] check if [reynolds-centOS7] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_Beta/CASREV=7.8,ESP_ARCH=LINUX64,buildnode=reynolds-centOS7 #723'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS