Started by upstream project "ESP_RegCaps" build number 679
originally caused by:
Started by an SCM change
Running as SYSTEM
[EnvInject] - Loading node environment variables.
Building remotely on macys in workspace /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64
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U trunk/config/README.txt
U trunk/config/setup.command
U trunk/config/setup.sh
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U training/2023/data/session10/2_aeroelastic_Iterative_SU2_Astros.py
U training/2023/data/session07/12_aflr4_aflr3_ViscousTransport.py
A training/lectures
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A training/lectures/session02.tex
A training/lectures/CAPSoptions.tex
A training/lectures/session08.tex
A training/lectures/Makefile
A training/lectures/muddy_06_07.tex
A training/lectures/muddy_08_09.tex
A training/lectures/session09.tex
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A training/lectures/MUDDYoptions.tex
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A training/lectures/welcome.tex
A training/lectures/session06
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A training/lectures/session05
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A training/lectures/session05/plane.avl
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A training/lectures/session07
AU training/lectures/session07/inviscidWingPod_SourceSpace1.png
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A training/lectures/session09
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A training/lectures/session10
AU training/lectures/session10/capsLoad.png
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A training/lectures/session11
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AU training/lectures/session11/vertexSet_Aero_upperWing.png
AU training/lectures/session11/vertexSet_Struct_upperWing.png
A training/lectures/CAPSflyer.tex
A training/lectures/session04.tex
A training/lectures/welcome
AU training/lectures/welcome/AFRL.png
AU training/lectures/welcome/DARPA.png
AU training/lectures/welcome/NASA.png
A training/lectures/session04
A training/lectures/session04/save.view
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AU training/lectures/session04/wing4_CFDvisc.png
AU training/lectures/session04/wing4_VLM.png
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AU training/lectures/session04/transport.png
AU training/lectures/session04/wing1.png
A training/lectures/csmListing.tex
A training/lectures/csmListingsBW.tex
A training/lectures/session01
AU training/lectures/session01/ParaView_Logo.png
AU training/lectures/session01/AIMdoc.png
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A training/lectures/session08
A training/lectures/session08/logoSU2_v3_3_mod.png
AU training/lectures/session08/hi_lift2.jpg
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AU training/lectures/session08/fun3d_logo.png
AU training/lectures/session08/nasa_meatball_0138.png
AU training/lectures/cmpress
A training/lectures/PythonTutorial.tex
A training/lectures/session02
AU training/lectures/session02/f118_boxter.png
A training/lectures/session03
AU training/lectures/session03/avl_logo.png
AU training/lectures/session03/naca.png
AU training/lectures/session03/planevanilla.png
AU training/lectures/session03/xfoil_logo.png
A training/lectures/capsSyllabus.tex
A training/lectures/oneTrainingSyllabus.tex
AU training/lectures/questionnaire.docx
A training/lectures/syllabus.tex
A training/lectures/cover.tex
A training/lectures/overlayPageSubNumber.tex
A training/lectures/ParaviewBasics
AU training/lectures/ParaviewBasics/basic_paraview.pdf
AU training/lectures/ParaviewBasics/basic_paraview.pptx
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A training/lectures/BEAMERoptions.tex
A training/lectures/CAPSauthor.tex
AU training/lectures/caps_logo.png
A training/lectures/beamercolorthemeesp.sty
AU training/lectures/esp_logo.png
A aim/unitTest/csmData/parsecSection.csm
At revision 4251
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U ESP_Env.sh
At revision 882
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A verify_7.8.1
A verify_7.8.1/CE13_LDI_Combustor_Test_Section_1.vfy
A verify_7.8.1/CE13_LDI_Combustor_Test_Section_2.vfy
A verify_7.8.1/CRM_NACA.vfy
A verify_7.8.1/Carrera.vfy
A verify_7.8.1/GEM_year1a.vfy
A verify_7.8.1/GEM_year1b.vfy
A verify_7.8.1/GEM_year1c.vfy
A verify_7.8.1/GEM_year2.vfy
A verify_7.8.1/M85_modified.vfy
A verify_7.8.1/RM-10.vfy
A verify_7.8.1/X29.vfy
A verify_7.8.1/afrl_wing1.vfy
A verify_7.8.1/afrl_wing2.vfy
A verify_7.8.1/afrl_wing3.vfy
A verify_7.8.1/bottle.vfy
A verify_7.8.1/bottle2.vfy
A verify_7.8.1/controlarm.vfy
A verify_7.8.1/fighter1.vfy
A verify_7.8.1/fighter2.vfy
A verify_7.8.1/fighter3.vfy
A verify_7.8.1/fighter4.vfy
A verify_7.8.1/grc_nozzle1.vfy
A verify_7.8.1/grc_nozzle9.vfy
A verify_7.8.1/jmr3a.vfy
A verify_7.8.1/jmr3b.vfy
A verify_7.8.1/jsc_config1.vfy
A verify_7.8.1/lander.vfy
A verify_7.8.1/lander_leg.vfy
A verify_7.8.1/partspanflap1.vfy
A verify_7.8.1/partspanflap2.vfy
A verify_7.8.1/spear0.vfy
A verify_7.8.1/spear1.vfy
A verify_7.8.1/tutorial1.vfy
A verify_7.8.1/tutorial2.vfy
A verify_7.8.1/tutorial3.vfy
A verify_7.8.1/tutorial4.vfy
A verify_7.8.1/tutorial5.vfy
A verify_7.8.1/wingbody.vfy
A Slugs
A Slugs/verify_7.8.1
A Slugs/verify_7.8.1/blend12_1.vfy
A Slugs/verify_7.8.1/blindeye_1.vfy
A Slugs/verify_7.8.1/boxBall_1.vfy
A Slugs/verify_7.8.1/boxHole_1.vfy
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A Slugs/verify_7.8.1/cylinderHole_1.vfy
A Slugs/verify_7.8.1/cylinder_1.vfy
A Slugs/verify_7.8.1/damaged_2.vfy
A Slugs/verify_7.8.1/demo1_1.vfy
A Slugs/verify_7.8.1/duct_1.vfy
A Slugs/verify_7.8.1/eyeball_1.vfy
A Slugs/verify_7.8.1/holes_1.vfy
A Slugs/verify_7.8.1/pieslice_1.vfy
A Slugs/verify_7.8.1/sphere_1.vfy
A Slugs/verify_7.8.1/torus_1.vfy
A Slugs/verify_7.8.1/tutorial1.vfy
A Slugs/verify_7.8.1/wing_1.vfy
A Slugs/verify_7.8.0
A Slugs/verify_7.8.0/blend12_1.vfy
A Slugs/verify_7.8.0/blindeye_1.vfy
A Slugs/verify_7.8.0/boxBall_1.vfy
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A Slugs/verify_7.8.0/demo1_1.vfy
A Slugs/verify_7.8.0/duct_1.vfy
A Slugs/verify_7.8.0/eyeball_1.vfy
A Slugs/verify_7.8.0/holes_1.vfy
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A Slugs/verify_7.8.0/wing_1.vfy
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A Slugs/verify_7.7.0/demo1_1.vfy
A Slugs/verify_7.7.0/duct_1.vfy
A Slugs/verify_7.7.0/eyeball_1.vfy
A Slugs/verify_7.7.0/holes_1.vfy
A Slugs/verify_7.7.0/pieslice_1.vfy
A Slugs/verify_7.7.0/sphere_1.vfy
A Slugs/verify_7.7.0/torus_1.vfy
A Slugs/verify_7.7.0/tutorial1.vfy
A Slugs/verify_7.7.0/wing_1.vfy
A Slugs/verify_7.6.0
A Slugs/verify_7.6.0/blend12_1.vfy
A Slugs/verify_7.6.0/blindeye_1.vfy
A Slugs/verify_7.6.0/boxBall_1.vfy
A Slugs/verify_7.6.0/boxHole_1.vfy
A Slugs/verify_7.6.0/box_1.vfy
A Slugs/verify_7.6.0/cylinderHole_1.vfy
A Slugs/verify_7.6.0/cylinder_1.vfy
A Slugs/verify_7.6.0/damaged_2.vfy
A Slugs/verify_7.6.0/demo1_1.vfy
A Slugs/verify_7.6.0/duct_1.vfy
A Slugs/verify_7.6.0/eyeball_1.vfy
A Slugs/verify_7.6.0/holes_1.vfy
A Slugs/verify_7.6.0/pieslice_1.vfy
A Slugs/verify_7.6.0/sphere_1.vfy
A Slugs/verify_7.6.0/torus_1.vfy
A Slugs/verify_7.6.0/tutorial1.vfy
A Slugs/verify_7.6.0/wing_1.vfy
A Slugs/holes_0.stl
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’
A Slugs/boxBall_0.jrnl
A Slugs/boxBall.plot
A Slugs/boxBall_0.stl
A Slugs/holes.plot
A Slugs/holes_0.csm
A Slugs/holes_0.jrnl
A Slugs/holes_1.csm
AU Slugs/tutorial1.stl
A Slugs/sphere_0.stl
A Slugs/blend12.plot
A Slugs/blend12_0.csm
A Slugs/blend12_0.stl
A Slugs/blindeye.plot
A Slugs/blindeye_0.csm
A Slugs/blindeye_0.jrnl
A Slugs/blindeye_0.stl
A Slugs/blindeye_1.csm
A Slugs/box.plot
A Slugs/boxBall_0.csm
A Slugs/boxBall_1.csm
A Slugs/boxHole.plot
A Slugs/boxHole_0.csm
A Slugs/boxHole_0.jrnl
A Slugs/boxHole_0.stl
A Slugs/box_0.csm
A Slugs/box_0.jrnl
A Slugs/box_0.stl
A Slugs/cylinder.plot
A Slugs/cylinderHole.plot
A Slugs/cylinderHole_0.csm
A Slugs/cylinderHole_0.jrnl
A Slugs/cylinderHole_0.stl
A Slugs/cylinder_0.csm
A Slugs/cylinder_0.jrnl
A Slugs/cylinder_0.stl
A Slugs/damaged.plot
A Slugs/damaged_0.csm
A Slugs/damaged_0.stl
A Slugs/damaged_1.jrnl
A Slugs/demo1.plot
A Slugs/demo1_0.csm
A Slugs/demo1_0.jrnl
A Slugs/demo1_0.stl
A Slugs/duct.plot
A Slugs/duct_0.csm
A Slugs/duct_0.jrnl
A Slugs/duct_0.stl
A Slugs/eyeball.plot
A Slugs/eyeball_0.csm
A Slugs/eyeball_0.jrnl
A Slugs/eyeball_0.stl
A Slugs/myGlider.plot
A Slugs/myGlider_0.cpc
A Slugs/myGlider_0.stl
A Slugs/pieslice.plot
A Slugs/pieslice_0.csm
A Slugs/pieslice_0.jrnl
A Slugs/pieslice_0.stl
A Slugs/sphere.plot
A Slugs/sphere_0.csm
A Slugs/sphere_0.jrnl
A Slugs/torus.plot
A Slugs/torus_0.csm
A Slugs/torus_0.jrnl
A Slugs/torus_0.stl
A Slugs/tutorial1.jrnl
A Slugs/tutorial1.plot
A Slugs/tutorial1_setup.csm
A Slugs/tutorial1_setup.stl
A Slugs/wing.plot
A Slugs/wingBody.plot
A Slugs/wingBody_0.cpc
A Slugs/wingBody_0.stl
A Slugs/wing_0.csm
A Slugs/wing_0.jrnl
A Slugs/wing_0.stl
A Slugs/blend12_1.csm
A Slugs/boxHole_1.csm
A Slugs/box_1.csm
A Slugs/cylinderHole_1.csm
A Slugs/cylinder_1.csm
A Slugs/damaged_2.csm
A Slugs/demo1_1.csm
A Slugs/duct_1.csm
A Slugs/myGlider_2.csm
A Slugs/sphere_1.csm
A Slugs/torus_1.csm
A Slugs/tutorial1.csm
A Slugs/wingBody_2.csm
A Slugs/wing_1.csm
A Slugs/testfiles
A Slugs/testfiles/elbow.stl
A Slugs/testfiles/elbow_NW.csm
A Slugs/testfiles/elbow_NW.jrnl
A Slugs/testfiles/elbow_NW.stl
A Slugs/testfiles/nucleus1.csm
A Slugs/testfiles/nucleus1.jrnl
A Slugs/testfiles/nucleus1.stl
A Slugs/testfiles/nucleus2.stl
A Slugs/testfiles/nucleus3.stl
AU Slugs/aneurysm_case1.iges
AU Slugs/aneurysm_case1_slugs.stl
A Slugs/eyeball_1.csm
A Slugs/pieslice_1.csm
A Slugs/myGlider_0.jrnl
A Slugs/myGlider_1.jrnl
A Slugs/damaged_0.jrnl
A Slugs/wingBody_0.jrnl
A Slugs/wingBody_1.jrnl
A Slugs/tutorial1_setup.jrnl
A Slugs/blend12_0.jrnl
At revision 2518
Cleaning up /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/OpenCSM/trunk/pyOCSM
Deleting /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/OpenCSM/trunk/pyOCSM/pyOCSM/__pycache__
Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/pyOCSM at revision '2024-07-27T22:19:12.228 -0400'
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 2518
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’
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’
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’
No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/src since the previous build
No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/udc since the previous build
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/pyOCSM 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 Windows batch command]
[Execution node] check if [macys] is in [[macys, macys_VM, reynolds, viggen]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[DARWIN64] $ /bin/bash -xe /var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/jenkins11463811669647049524.sh
+ rm -rf /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/training/lectures
+ [[ CAPS/AEROELASTIC != *\S\l\u\g\s* ]]
+ rm -rf /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/OpenCSM/trunk/data/Slugs
+ [[ macys == *\v\i\g\g\e\n* ]]
+ bash -ex /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/JenkinsESP/ESP_Regression.sh
+ source /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.8
++ OCCTREF=7.8
++ AFLR_VERSION=11.5.15
++ SU2_VERSION=8.0.1
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.38.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ export MPLBACKEND=agg
++ MPLBACKEND=agg
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ macys == \r\e\y\n\o\l\d\s ]]
++ [[ DARWIN64 == *\.\i\f\o\r\t ]]
++ '[' -f /opt/intel/oneapi/setvars.sh ']'
++ source /opt/intel/oneapi/setvars.sh
++ '[' -f /Users/jenkins/.bashrc ']'
++ export CAPS_OUTLEVEL=0
++ CAPS_OUTLEVEL=0
++ export ESP_UDC_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/OpenCSM/trunk/personalUdc
++ ESP_UDC_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/OpenCSM/trunk/personalUdc
++ [[ DARWIN64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64
++ ESP_BLOC=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64
++ ESP_ROOT=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64
++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/julia
++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.8 != '' ]]
++ [[ '' != '' ]]
++ [[ macys == *\r\e\y\n\o\l\d\s* ]]
++ [[ macys == *\m\a\c\y\s* ]]
++ export EMPnumProc=2
++ EMPnumProc=2
++ export OMP_NUM_THREADS=2
++ OMP_NUM_THREADS=2
++ source /Users/jenkins/.bash_profile
+++ export PATH=/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ PATH=/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ export PATH=/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ PATH=/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ export pwid_LICENSE=5053@acdl.mit.edu
+++ pwid_LICENSE=5053@acdl.mit.edu
++ [[ macys == *\m\a\c\y\s* ]]
++ export PATH=/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ [[ macys == \m\a\c\y\s ]]
++ echo 'data/fighter4.csm; ERROR:: build not completed because error -214 (did_not_create_body) was detected'
++ echo 'data/fighter4.csm; ERROR:: build not completed because error -214 (did_not_create_body) was detected'
++ echo 'data/fighter4.csm; ERROR:: build not completed because error -214 (did_not_create_body) was detected'
++ export CASARCH=.
++ CASARCH=.
++ '[' '!' -z '' ']'
+++ ls -d /Users/jenkins/util/ESP/OpenCASCADE-7.7.0
++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0
++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0
++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/udunits/udunits2.xml
++ export ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs
++ ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs
++ export DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/opt/intel/oneapi/tbb/2021.3.0/env/../lib:/opt/intel/oneapi/mkl/2021.3.0/lib:/opt/intel/oneapi/ipp/2021.3.0/lib:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib/intel64_mac:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib
++ DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/opt/intel/oneapi/tbb/2021.3.0/env/../lib:/opt/intel/oneapi/mkl/2021.3.0/lib:/opt/intel/oneapi/ipp/2021.3.0/lib:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib/intel64_mac:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib
++ export AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.15
++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.15
++ [[ macys == *\m\a\c\y\s* ]]
++ export AFLR_ARCH=MacOSX-x86-64
++ AFLR_ARCH=MacOSX-x86-64
++ export ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ export PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ export CART3D_ARCH=OSX64_ICC
++ CART3D_ARCH=OSX64_ICC
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS
++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ [[ macys == \m\a\c\y\s ]]
++ export SEACAS=/Users/jenkins/util/sandialabs/seacas
++ SEACAS=/Users/jenkins/util/sandialabs/seacas
++ [[ macys == \v\i\g\g\e\n ]]
++ export SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.1
++ SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.1
++ export SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ export PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ export PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']'
+++ perl -I/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5 -Mlocal::lib=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
++ eval 'PATH="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin${PATH:+:${PATH}}"; export PATH;
PERL5LIB="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5${PERL5LIB:+:${PERL5LIB}}"; export PERL5LIB;
PERL_LOCAL_LIB_ROOT="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl${PERL_LOCAL_LIB_ROOT:+:${PERL_LOCAL_LIB_ROOT}}"; export PERL_LOCAL_LIB_ROOT;
PERL_MB_OPT="--install_base \"/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl\""; export PERL_MB_OPT;
PERL_MM_OPT="INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"; export PERL_MM_OPT;'
+++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin
+++ export PATH
+++ PERL5LIB=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5
+++ export PERL5LIB
+++ PERL_LOCAL_LIB_ROOT=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
+++ export PERL_LOCAL_LIB_ROOT
+++ PERL_MB_OPT='--install_base "/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"'
+++ export PERL_MB_OPT
+++ PERL_MM_OPT=INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
+++ export PERL_MM_OPT
++ export PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ export PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ [[ macys == \m\a\c\y\s* ]]
++ mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin
++ rm -f /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/python
++ rm -f /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/python-config
++ rm -f /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/virtualenv
++ rm -f '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/analyze-*'
++ rm -f '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/intercept-*'
++ [[ macys == \m\a\c\y\s ]]
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/python
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3-config /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/python-config
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/virtualenv /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/virtualenv
+++ ls /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/analyze-build
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/analyze-c++
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/analyze-cc
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/intercept-build
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/intercept-c++
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/intercept-cc
+++ python-config --includes
++ export 'PYTHONINC=. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
++ PYTHONINC='. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
+++ python-config --help
++ [[ Usage: /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/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/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation'
++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation'
++ [[ macys == \m\a\c\y\s ]]
++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w'
++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w'
++ export PYTHONUNBUFFERED=true
++ PYTHONUNBUFFERED=true
++ export PYTHONFAULTHANDLER=true
++ PYTHONFAULTHANDLER=true
++ python --version
Python 3.11.9
++ [[ DARWIN64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export CSMDATA=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/OpenCSM/trunk/data
++ CSMDATA=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/OpenCSM/trunk/data
+ source /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/JenkinsESP/ESPbfr.sh
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/
++ tar -xvf /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/JenkinsESP/ESPbfr.tgz
x ESP/
x ESP/CYGWIN64/
x ESP/CYGWIN64/bin/
x ESP/CYGWIN64/bin/mastros.exe
x ESP/CYGWIN64/bin/ASTRO.D01
x ESP/CYGWIN64/bin/ASTRO.IDX
x ESP/CYGWIN64/include/
x ESP/CYGWIN64/lib/
x ESP/CYGWIN64/lib/libquadmath-0.dll
x ESP/CYGWIN64/lib/libwinpthread-1.dll
x ESP/CYGWIN64/lib/libgcc_s_sjlj-1.dll
x ESP/CYGWIN64/obj/
x ESP/CYGWIN64/test/
x ESP/DARWIN64/
x ESP/DARWIN64/bin/
x ESP/DARWIN64/bin/mastros.exe
x ESP/DARWIN64/bin/ASTRO.D01
x ESP/DARWIN64/bin/mset
x ESP/DARWIN64/bin/ASTRO.IDX
x ESP/DARWIN64/bin/avl
x ESP/DARWIN64/bin/xfoil
x ESP/DARWIN64/bin/mses
x ESP/DARWIN64/include/
x ESP/DARWIN64/include/nmb.h
x ESP/DARWIN64/include/xddm/
x ESP/DARWIN64/include/xddm/xddmInternals.h
x ESP/DARWIN64/include/xddm/xddm.h
x ESP/DARWIN64/include/xddm/xddm.c
x ESP/DARWIN64/include/converter.h
x ESP/DARWIN64/include/libCart3D/
x ESP/DARWIN64/include/libCart3D/sensors.h
x ESP/DARWIN64/include/libCart3D/SFC.h
x ESP/DARWIN64/include/libCart3D/map.h
x ESP/DARWIN64/include/libCart3D/MGinfo.h
x ESP/DARWIN64/include/libCart3D/gridStructures.h
x ESP/DARWIN64/include/libCart3D/timer.h
x ESP/DARWIN64/include/libCart3D/ConvInfo.h
x ESP/DARWIN64/include/libCart3D/dualtime.h
x ESP/DARWIN64/include/libCart3D/stateVector.h
x ESP/DARWIN64/include/libCart3D/cartCells.h
x ESP/DARWIN64/include/libCart3D/encoding.h
x ESP/DARWIN64/include/libCart3D/string_util.h
x ESP/DARWIN64/include/libCart3D/int64.h
x ESP/DARWIN64/include/libCart3D/bBox_stuff.h
x ESP/DARWIN64/include/libCart3D/basicTypes.h
x ESP/DARWIN64/include/libCart3D/utils_xml.h
x ESP/DARWIN64/include/libCart3D/hex.h
x ESP/DARWIN64/include/libCart3D/PostProcInfo.h
x ESP/DARWIN64/include/libCart3D/SolverInfo.h
x ESP/DARWIN64/include/libCart3D/earthBL_BC.h
x ESP/DARWIN64/include/libCart3D/limiters.h
x ESP/DARWIN64/include/libCart3D/geomStructures.h
x ESP/DARWIN64/include/libCart3D/CaseInfo.h
x ESP/DARWIN64/include/libCart3D/memory_util.h
x ESP/DARWIN64/include/libCart3D/infoStructures.h
x ESP/DARWIN64/include/libCart3D/geomTypes.h
x ESP/DARWIN64/include/libCart3D/c3d_timeout.h
x ESP/DARWIN64/include/libCart3D/myLList.h
x ESP/DARWIN64/include/libCart3D/IOinfo.h
x ESP/DARWIN64/include/libCart3D/GridInfo.h
x ESP/DARWIN64/include/libCart3D/c3d_global.h
x ESP/DARWIN64/include/libCart3D/vortexBC.h
x ESP/DARWIN64/include/c3dio/
x ESP/DARWIN64/include/c3dio/c3dio_icemcfd.h
x ESP/DARWIN64/include/c3dio/c3dio_lib.h
x ESP/DARWIN64/include/udunits.h
x ESP/DARWIN64/include/udunits2.h
x ESP/DARWIN64/lib/
x ESP/DARWIN64/lib/libudunits2.dylib
x ESP/DARWIN64/lib/libudunits2.0.dylib
x ESP/DARWIN64/lib/libCart3D.a
x ESP/DARWIN64/lib/libnmb.dylib
x ESP/DARWIN64/lib/libc3dio.a
x ESP/DARWIN64/obj/
x ESP/DARWIN64/test/
x ESP/DARWIN_ARM64/
x ESP/DARWIN_ARM64/bin/
x ESP/DARWIN_ARM64/bin/mastros.exe
x ESP/DARWIN_ARM64/bin/ASTRO.D01
x ESP/DARWIN_ARM64/bin/mset
x ESP/DARWIN_ARM64/bin/ASTRO.IDX
x ESP/DARWIN_ARM64/bin/avl
x ESP/DARWIN_ARM64/bin/xfoil
x ESP/DARWIN_ARM64/bin/mses
x ESP/DARWIN_ARM64/include/
x ESP/DARWIN_ARM64/include/nmb.h
x ESP/DARWIN_ARM64/include/xddm/
x ESP/DARWIN_ARM64/include/xddm/xddmInternals.h
x ESP/DARWIN_ARM64/include/xddm/xddm.h
x ESP/DARWIN_ARM64/include/xddm/xddm.c
x ESP/DARWIN_ARM64/include/converter.h
x ESP/DARWIN_ARM64/include/libCart3D/
x ESP/DARWIN_ARM64/include/libCart3D/sensors.h
x ESP/DARWIN_ARM64/include/libCart3D/SFC.h
x ESP/DARWIN_ARM64/include/libCart3D/map.h
x ESP/DARWIN_ARM64/include/libCart3D/MGinfo.h
x ESP/DARWIN_ARM64/include/libCart3D/gridStructures.h
x ESP/DARWIN_ARM64/include/libCart3D/timer.h
x ESP/DARWIN_ARM64/include/libCart3D/ConvInfo.h
x ESP/DARWIN_ARM64/include/libCart3D/dualtime.h
x ESP/DARWIN_ARM64/include/libCart3D/stateVector.h
x ESP/DARWIN_ARM64/include/libCart3D/cartCells.h
x ESP/DARWIN_ARM64/include/libCart3D/encoding.h
x ESP/DARWIN_ARM64/include/libCart3D/string_util.h
x ESP/DARWIN_ARM64/include/libCart3D/int64.h
x ESP/DARWIN_ARM64/include/libCart3D/bBox_stuff.h
x ESP/DARWIN_ARM64/include/libCart3D/basicTypes.h
x ESP/DARWIN_ARM64/include/libCart3D/utils_xml.h
x ESP/DARWIN_ARM64/include/libCart3D/hex.h
x ESP/DARWIN_ARM64/include/libCart3D/PostProcInfo.h
x ESP/DARWIN_ARM64/include/libCart3D/SolverInfo.h
x ESP/DARWIN_ARM64/include/libCart3D/earthBL_BC.h
x ESP/DARWIN_ARM64/include/libCart3D/limiters.h
x ESP/DARWIN_ARM64/include/libCart3D/geomStructures.h
x ESP/DARWIN_ARM64/include/libCart3D/CaseInfo.h
x ESP/DARWIN_ARM64/include/libCart3D/memory_util.h
x ESP/DARWIN_ARM64/include/libCart3D/infoStructures.h
x ESP/DARWIN_ARM64/include/libCart3D/geomTypes.h
x ESP/DARWIN_ARM64/include/libCart3D/c3d_timeout.h
x ESP/DARWIN_ARM64/include/libCart3D/myLList.h
x ESP/DARWIN_ARM64/include/libCart3D/IOinfo.h
x ESP/DARWIN_ARM64/include/libCart3D/GridInfo.h
x ESP/DARWIN_ARM64/include/libCart3D/c3d_global.h
x ESP/DARWIN_ARM64/include/libCart3D/vortexBC.h
x ESP/DARWIN_ARM64/include/c3dio/
x ESP/DARWIN_ARM64/include/c3dio/c3dio_icemcfd.h
x ESP/DARWIN_ARM64/include/c3dio/c3dio_lib.h
x ESP/DARWIN_ARM64/include/udunits.h
x ESP/DARWIN_ARM64/include/udunits2.h
x ESP/DARWIN_ARM64/lib/
x ESP/DARWIN_ARM64/lib/libudunits2.dylib
x ESP/DARWIN_ARM64/lib/libudunits2.0.dylib
x ESP/DARWIN_ARM64/lib/libCart3D.a
x ESP/DARWIN_ARM64/lib/libc3dio.a
x ESP/DARWIN_ARM64/obj/
x ESP/DARWIN_ARM64/test/
x ESP/LINUX64/
x ESP/LINUX64/bin/
x ESP/LINUX64/bin/mastros.exe
x ESP/LINUX64/bin/ASTRO.D01
x ESP/LINUX64/bin/mset
x ESP/LINUX64/bin/ASTRO.IDX
x ESP/LINUX64/bin/avl
x ESP/LINUX64/bin/xfoil
x ESP/LINUX64/bin/mses
x ESP/LINUX64/include/
x ESP/LINUX64/include/nmb.h
x ESP/LINUX64/include/xddm/
x ESP/LINUX64/include/xddm/xddmInternals.h
x ESP/LINUX64/include/xddm/xddm.h
x ESP/LINUX64/include/xddm/xddm.c
x ESP/LINUX64/include/libCart3D/
x ESP/LINUX64/include/libCart3D/sensors.h
x ESP/LINUX64/include/libCart3D/SFC.h
x ESP/LINUX64/include/libCart3D/map.h
x ESP/LINUX64/include/libCart3D/MGinfo.h
x ESP/LINUX64/include/libCart3D/gridStructures.h
x ESP/LINUX64/include/libCart3D/timer.h
x ESP/LINUX64/include/libCart3D/ConvInfo.h
x ESP/LINUX64/include/libCart3D/dualtime.h
x ESP/LINUX64/include/libCart3D/stateVector.h
x ESP/LINUX64/include/libCart3D/cartCells.h
x ESP/LINUX64/include/libCart3D/encoding.h
x ESP/LINUX64/include/libCart3D/string_util.h
x ESP/LINUX64/include/libCart3D/int64.h
x ESP/LINUX64/include/libCart3D/bBox_stuff.h
x ESP/LINUX64/include/libCart3D/basicTypes.h
x ESP/LINUX64/include/libCart3D/utils_xml.h
x ESP/LINUX64/include/libCart3D/hex.h
x ESP/LINUX64/include/libCart3D/PostProcInfo.h
x ESP/LINUX64/include/libCart3D/SolverInfo.h
x ESP/LINUX64/include/libCart3D/earthBL_BC.h
x ESP/LINUX64/include/libCart3D/limiters.h
x ESP/LINUX64/include/libCart3D/geomStructures.h
x ESP/LINUX64/include/libCart3D/CaseInfo.h
x ESP/LINUX64/include/libCart3D/memory_util.h
x ESP/LINUX64/include/libCart3D/infoStructures.h
x ESP/LINUX64/include/libCart3D/geomTypes.h
x ESP/LINUX64/include/libCart3D/c3d_timeout.h
x ESP/LINUX64/include/libCart3D/myLList.h
x ESP/LINUX64/include/libCart3D/IOinfo.h
x ESP/LINUX64/include/libCart3D/GridInfo.h
x ESP/LINUX64/include/libCart3D/c3d_global.h
x ESP/LINUX64/include/libCart3D/vortexBC.h
x ESP/LINUX64/include/c3dio/
x ESP/LINUX64/include/c3dio/c3dio_icemcfd.h
x ESP/LINUX64/include/c3dio/c3dio_lib.h
x ESP/LINUX64/lib/
x ESP/LINUX64/lib/libnmb.so
x ESP/LINUX64/lib/libCart3D.a
x ESP/LINUX64/lib/libc3dio.a
x ESP/LINUX64/obj/
x ESP/LINUX64/test/
x ESP/WIN64/
x ESP/WIN64/bin/
x ESP/WIN64/bin/mses.exe
x ESP/WIN64/bin/avl.exe
x ESP/WIN64/bin/mastros.exe
x ESP/WIN64/bin/ASTRO.D01
x ESP/WIN64/bin/xfoil.exe
x ESP/WIN64/bin/ASTRO.IDX
x ESP/WIN64/bin/mset.exe
x ESP/WIN64/include/
x ESP/WIN64/include/nmb.h
x ESP/WIN64/include/winhelpers/
x ESP/WIN64/include/winhelpers/gettimeofday.h
x ESP/WIN64/include/winhelpers/websock-w32.h
x ESP/WIN64/include/winhelpers/netdb.h
x ESP/WIN64/include/winhelpers/unistd.h
x ESP/WIN64/include/winhelpers/strings.h
x ESP/WIN64/include/winhelpers/sys/
x ESP/WIN64/include/winhelpers/sys/time.h
x ESP/WIN64/include/converter.h
x ESP/WIN64/include/udunits.h
x ESP/WIN64/include/udunits2.h
x ESP/WIN64/lib/
x ESP/WIN64/lib/libquadmath-0.dll
x ESP/WIN64/lib/nmb.lib
x ESP/WIN64/lib/libwinpthread-1.dll
x ESP/WIN64/lib/udunits2.lib
x ESP/WIN64/lib/libgcc_s_sjlj-1.dll
x ESP/WIN64/lib/expat.dll
x ESP/WIN64/lib/udunits2.dll
x ESP/WIN64/lib/nmb.dll
x ESP/WIN64/obj/
x ESP/WIN64/test/
x ESP/LINUX_AARCH64/
x ESP/LINUX_AARCH64/bin/
x ESP/LINUX_AARCH64/bin/mastros.exe
x ESP/LINUX_AARCH64/bin/ASTRO.D01
x ESP/LINUX_AARCH64/bin/mset
x ESP/LINUX_AARCH64/bin/ASTRO.IDX
x ESP/LINUX_AARCH64/bin/avl
x ESP/LINUX_AARCH64/bin/xfoil
x ESP/LINUX_AARCH64/bin/mses
x ESP/LINUX_AARCH64/include/
x ESP/LINUX_AARCH64/lib/
x ESP/LINUX_AARCH64/obj/
x ESP/LINUX_AARCH64/test/
x ESP/udunits/
x ESP/udunits/udunits2-accepted.xml
x ESP/udunits/udunits2-base.xml
x ESP/udunits/udunits2-common.xml
x ESP/udunits/udunits2.xml
x ESP/udunits/udunits2-derived.xml
x ESP/udunits/udunits2-prefixes.xml
++ virtualenv --system-site-packages /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv
created virtual environment CPython3.11.9.final.0-64 in 417ms
creator CPython3Posix(dest=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv, clear=False, no_vcs_ignore=False, global=True)
seeder FromAppData(download=False, pip=bundle, setuptools=bundle, wheel=bundle, via=copy, app_data_dir=/Users/jenkins/Library/Application Support/virtualenv)
added seed packages: pip==24.1.2, setuptools==70.1.1, wheel==0.43.0
activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator
++ . /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv/bin/activate
+++ '[' /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv/bin/activate = /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/JenkinsESP/ESP_Regression.sh ']'
+++ deactivate nondestructive
+++ unset -f pydoc
+++ '[' -z '' ']'
+++ '[' -z '' ']'
+++ hash -r
+++ '[' -z '' ']'
+++ unset VIRTUAL_ENV
+++ unset VIRTUAL_ENV_PROMPT
+++ '[' '!' nondestructive = nondestructive ']'
+++ VIRTUAL_ENV=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv
+++ '[' darwin22 = cygwin ']'
+++ '[' darwin22 = msys ']'
+++ export VIRTUAL_ENV
+++ _OLD_VIRTUAL_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin
+++ PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv/bin:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin
+++ export PATH
+++ '[' x '!=' x ']'
++++ basename /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv
+++ VIRTUAL_ENV_PROMPT=venv
+++ export VIRTUAL_ENV_PROMPT
+++ '[' -z '' ']'
+++ '[' -z '' ']'
+++ _OLD_VIRTUAL_PS1=
+++ PS1='(venv) '
+++ export PS1
+++ alias pydoc
+++ true
+++ hash -r
++ pip_install pip
++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade pip
Requirement already satisfied: pip in ./ESP/venv/lib/python3.11/site-packages (24.1.2)
++ pip_install f90nml
++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade f90nml
Requirement already satisfied: f90nml in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (1.4.4)
++ pip_install numpy
++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade numpy
Requirement already satisfied: numpy in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (1.26.4)
Collecting numpy
Using cached numpy-2.0.1-cp311-cp311-macosx_10_9_x86_64.whl.metadata (60 kB)
Using cached numpy-2.0.1-cp311-cp311-macosx_10_9_x86_64.whl (21.2 MB)
Installing collected packages: numpy
Attempting uninstall: numpy
Found existing installation: numpy 1.26.4
Not uninstalling numpy at /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages, outside environment /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv
Can't uninstall 'numpy'. No files were found to uninstall.
ERROR: pip's dependency resolver does not currently take into account all the packages that are installed. This behaviour is the source of the following dependency conflicts.
openmdao 3.33.0 requires numpy<2, but you have numpy 2.0.1 which is incompatible.
pynastran 1.4.1 requires numpy<2, but you have numpy 2.0.1 which is incompatible.
numba 0.59.1 requires numpy<1.27,>=1.22, but you have numpy 2.0.1 which is incompatible.
tacs 3.7.2 requires numpy<2.0.0, but you have numpy 2.0.1 which is incompatible.
Successfully installed numpy-2.0.1
++ pip_install 'scipy!=1.9.2,!=1.9.3'
++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade 'scipy!=1.9.2,!=1.9.3'
Requirement already satisfied: scipy!=1.9.2,!=1.9.3 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (1.13.1)
Collecting scipy!=1.9.2,!=1.9.3
Using cached scipy-1.14.0-cp311-cp311-macosx_10_9_x86_64.whl.metadata (60 kB)
Requirement already satisfied: numpy<2.3,>=1.23.5 in ./ESP/venv/lib/python3.11/site-packages (from scipy!=1.9.2,!=1.9.3) (2.0.1)
Using cached scipy-1.14.0-cp311-cp311-macosx_10_9_x86_64.whl (39.1 MB)
Installing collected packages: scipy
Attempting uninstall: scipy
Found existing installation: scipy 1.13.1
Not uninstalling scipy at /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages, outside environment /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv
Can't uninstall 'scipy'. No files were found to uninstall.
ERROR: pip's dependency resolver does not currently take into account all the packages that are installed. This behaviour is the source of the following dependency conflicts.
openmdao 3.33.0 requires numpy<2, but you have numpy 2.0.1 which is incompatible.
pynastran 1.4.1 requires numpy<2, but you have numpy 2.0.1 which is incompatible.
tacs 3.7.2 requires numpy<2.0.0, but you have numpy 2.0.1 which is incompatible.
Successfully installed scipy-1.14.0
++ pip_install openmdao
++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade openmdao
Requirement already satisfied: openmdao in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (3.33.0)
Collecting openmdao
Using cached openmdao-3.34.2-py3-none-any.whl
Requirement already satisfied: networkx>=2.0 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from openmdao) (3.3)
Collecting numpy<2 (from openmdao)
Using cached numpy-1.26.4-cp311-cp311-macosx_10_9_x86_64.whl.metadata (61 kB)
Requirement already satisfied: packaging in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from openmdao) (24.0)
Requirement already satisfied: requests in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from openmdao) (2.32.3)
Requirement already satisfied: scipy in ./ESP/venv/lib/python3.11/site-packages (from openmdao) (1.14.0)
Requirement already satisfied: charset-normalizer<4,>=2 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from requests->openmdao) (3.3.2)
Requirement already satisfied: idna<4,>=2.5 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from requests->openmdao) (3.7)
Requirement already satisfied: urllib3<3,>=1.21.1 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from requests->openmdao) (2.2.1)
Requirement already satisfied: certifi>=2017.4.17 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from requests->openmdao) (2024.6.2)
Using cached numpy-1.26.4-cp311-cp311-macosx_10_9_x86_64.whl (20.6 MB)
Installing collected packages: numpy, openmdao
Attempting uninstall: numpy
Found existing installation: numpy 2.0.1
Uninstalling numpy-2.0.1:
Successfully uninstalled numpy-2.0.1
Attempting uninstall: openmdao
Found existing installation: openmdao 3.33.0
Not uninstalling openmdao at /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages, outside environment /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv
Can't uninstall 'openmdao'. No files were found to uninstall.
Successfully installed numpy-1.26.4 openmdao-3.34.2
++ [[ macys == *\v\i\g\g\e\n* ]]
++ pip_install cvxopt
++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade cvxopt
Requirement already satisfied: cvxopt in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (1.3.2)
++ pip_install dill
++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade dill
Requirement already satisfied: dill in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (0.3.8)
++ pip_install packaging
++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade packaging
Requirement already satisfied: packaging in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (24.0)
Collecting packaging
Using cached packaging-24.1-py3-none-any.whl.metadata (3.2 kB)
Using cached packaging-24.1-py3-none-any.whl (53 kB)
Installing collected packages: packaging
Attempting uninstall: packaging
Found existing installation: packaging 24.0
Not uninstalling packaging at /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages, outside environment /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv
Can't uninstall 'packaging'. No files were found to uninstall.
Successfully installed packaging-24.1
++ pip_install matplotlib
++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade matplotlib
Requirement already satisfied: matplotlib in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (3.9.0)
Collecting matplotlib
Using cached matplotlib-3.9.1-cp311-cp311-macosx_10_12_x86_64.whl.metadata (11 kB)
Requirement already satisfied: contourpy>=1.0.1 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from matplotlib) (1.2.1)
Requirement already satisfied: cycler>=0.10 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from matplotlib) (0.12.1)
Requirement already satisfied: fonttools>=4.22.0 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from matplotlib) (4.53.0)
Requirement already satisfied: kiwisolver>=1.3.1 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from matplotlib) (1.4.5)
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)
Requirement already satisfied: pillow>=8 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from matplotlib) (10.3.0)
Requirement already satisfied: pyparsing>=2.3.1 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from matplotlib) (3.1.2)
Requirement already satisfied: python-dateutil>=2.7 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from matplotlib) (2.9.0.post0)
Requirement already satisfied: six>=1.5 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from python-dateutil>=2.7->matplotlib) (1.16.0)
Using cached matplotlib-3.9.1-cp311-cp311-macosx_10_12_x86_64.whl (7.9 MB)
Installing collected packages: matplotlib
Attempting uninstall: matplotlib
Found existing installation: matplotlib 3.9.0
Not uninstalling matplotlib at /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages, outside environment /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv
Can't uninstall 'matplotlib'. No files were found to uninstall.
Successfully installed matplotlib-3.9.1
++ [[ /Users/jenkins/util/ESP/ExternLibs == '' ]]
++ '[' -d /Users/jenkins/util/ESP/ExternLibs ']'
++ cp /Users/jenkins/util/ESP/ExternLibs/intersectWake.so /Users/jenkins/util/ESP/ExternLibs/markWakeEdges.so /Users/jenkins/util/ESP/ExternLibs/sansLIPAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/EGADS/trunk/src
++ make
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/DARWIN64
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/DARWIN64
cp -p ../include/DARWIN64 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/DARWIN64
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/STANALYZER.make
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/STANALYZER.make
cp -p ../include/STANALYZER.make /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/STANALYZER.make
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egads.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egads.h
cp -p ../include/egads.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egads.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egads_dot.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egads_dot.h
cp -p ../include/egads_dot.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egads_dot.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egads.inc
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egads.inc
cp -p ../include/egads.inc /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egads.inc
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egadsErrors.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egadsErrors.h
cp -p ../include/egadsErrors.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egadsErrors.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egadsTypes.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egadsTypes.h
cp -p ../include/egadsTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egadsTypes.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/emp.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/emp.h
cp -p ../include/emp.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/emp.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/prm.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/prm.h
cp -p ../include/prm.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/prm.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/wsserver.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/wsserver.h
cp -p ../include/wsserver.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/wsserver.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/wsserver.inc
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/wsserver.inc
cp -p ../include/wsserver.inc /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/wsserver.inc
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/wsss.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/wsss.h
cp -p ../include/wsss.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/wsss.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egadsTris.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egadsTris.h
cp -p egadsTris.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egadsTris.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egadsSplineFit.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egadsSplineFit.h
cp -p egadsSplineFit.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egadsSplineFit.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egadsSplineVels.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egadsSplineVels.h
cp -p egadsSplineVels.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egadsSplineVels.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egadsf90.inc
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egadsf90.inc
cp -p ../include/egadsf90.inc /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egadsf90.inc
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/Surreal
cp Surreal/SurrealD.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/Surreal/SurrealD.h
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/Surreal
cp Surreal/SurrealD_Lazy.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/Surreal/SurrealD_Lazy.h
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/Surreal
cp Surreal/SurrealD_Trad.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/Surreal/SurrealD_Trad.h
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/Surreal
cp Surreal/SurrealS.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/Surreal/SurrealS.h
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/Surreal
cp Surreal/SurrealS_Lazy.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/Surreal/SurrealS_Lazy.h
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/Surreal
cp Surreal/SurrealS_Trad.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/Surreal/SurrealS_Trad.h
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/Surreal
cp Surreal/always_inline.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/Surreal/always_inline.h
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsGeom.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsGeom.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsHLevel.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsHLevel.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsTopo.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsTopo.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsCopy.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsCopy.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsSpline.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsSpline.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsIO.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsIO.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsSplineFit.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsSplineFit.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsSkinning.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsSkinning.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsTessSens.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsTessSens.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 OCC/BRepLib_FuseEdges.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/BRepLib_FuseEdges.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsBase.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsMemory.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsMemory.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsAttrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsAttrs.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsTess.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsTessInp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsTessInp.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsTris.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsTris.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsQuads.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsFit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsFit.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsRobust.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsRobust.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsSBO.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsSBO.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap prmCfit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/prmCfit.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap prmGrid.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/prmGrid.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap prmUV.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/prmUV.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsExport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsExport.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsEffect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsEffect.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsSolids.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsSolids.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include ../util/emp.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/emp.o
clang++ -g -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I. -I../include \
../util/evaluate.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/evaluate.o
clang++ -g -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I. -I../include \
../util/rational.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/rational.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -I../util \
../util/regQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/regQuads.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/SurrealD1
SurrealD1_test_suite Complete!
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/SurrealD4 -O -std=c++11 -I. ../util/SurrealD4_btest.cpp
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/SurrealD4
SurrealD4_test_suite Complete!
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/SurrealS1 -O -std=c++11 -I. ../util/SurrealS1_btest.cpp
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/SurrealS1
SurrealS1_test_suite Complete!
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/SurrealS4 -O -std=c++11 -I. ../util/SurrealS4_btest.cpp
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/SurrealS4
SurrealS4_test_suite Complete!
/Library/Developer/CommandLineTools/usr/bin/make -C ../util
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 uvmap/main/uvmap.c -Iuvmap \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapFindUV.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/EG_uvmapFindUV.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapGen.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/EG_uvmapGen.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapStructFree.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/EG_uvmapStructFree.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/EG_uvmapTest.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmap_Read.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/EG_uvmap_Read.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmap_Write.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/EG_uvmap_Write.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_add.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_add.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_bnd_adj.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_bnd_adj.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_chk_area_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_chk_area_uv.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_chk_edge_ratio.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_chk_edge_ratio.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_cpu_message.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_cpu_message.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_find_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_find_uv.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_from_egads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_from_egads.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_gen.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_gen.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_gen_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_gen_uv.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_ibeibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_ibeibe.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_ibfibf.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_ibfibf.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_ibfin.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_ibfin.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_iccibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_iccibe.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_iccin.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_iccin.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_idibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_idibe.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_inibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_inibe.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_inl_uv_bnd.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_inl_uv_bnd.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_malloc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_malloc.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_mben_disc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_mben_disc.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_message.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_message.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_norm_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_norm_uv.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_read.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_read.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_solve.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_solve.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_struct_tasks.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_struct_tasks.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_test.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_test.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_to_egads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_to_egads.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_version.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_version.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_write.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap_write.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 egadsUVmap.c -Iuvmap \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsUVmap.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libuvmap.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libuvmap.a
(cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libuvmap.a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsUVmap.o EG_uvmapFindUV.o EG_uvmapGen.o EG_uvmapStructFree.o EG_uvmapTest.o EG_uvmap_Read.o EG_uvmap_Write.o uvmap_add.o uvmap_bnd_adj.o uvmap_chk_area_uv.o uvmap_chk_edge_ratio.o uvmap_cpu_message.o uvmap_find_uv.o uvmap_from_egads.o uvmap_gen.o uvmap_gen_uv.o uvmap_ibeibe.o uvmap_ibfibf.o uvmap_ibfin.o uvmap_iccibe.o uvmap_iccin.o uvmap_idibe.o uvmap_inibe.o uvmap_inl_uv_bnd.o uvmap_malloc.o uvmap_mben_disc.o uvmap_message.o uvmap_norm_uv.o uvmap_read.o uvmap_solve.o uvmap_struct_tasks.o uvmap_test.o uvmap_to_egads.o uvmap_version.o uvmap_write.o; )
ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libuvmap.a
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/uvmap.exe /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/uvmap.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -luvmap -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libegads.dylib
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libegads.dylib
(cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libegads.dylib 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 \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet -lc++ \
-install_name '@rpath/libegads.dylib' \
-compatibility_version 7.7 \
-current_version 1.0.26 )
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libegadstatic.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libegadstatic.a
cp /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libuvmap.a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libegadstatic.a
(cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj; \
ar rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/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; )
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fgadsBase.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsMemory.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fgadsMemory.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsAttrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fgadsAttrs.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fgadsTess.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsHLevel.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fgadsHLevel.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsGeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fgadsGeom.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsTopo.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fgadsTopo.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libfgads.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libfgads.a
(cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libfgads.a fgadsBase.o fgadsMemory.o fgadsAttrs.o fgadsTess.o fgadsHLevel.o fgadsGeom.o fgadsTopo.o; )
ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libfgads.a
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libemp.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libemp.a
(cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libemp.a emp.o; )
ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libemp.a
*** EGADS Build Complete! ***
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/EGADS/trunk/wvServer
++ make
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 map.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/map.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include base64-decode.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/base64-decode.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include handshake.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/handshake.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include client-handshake.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/client-handshake.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include libwebsockets.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/libwebsockets.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include extension-deflate-stream.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/extension-deflate-stream.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include md5.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/md5.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include extension-x-google-mux.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/extension-x-google-mux.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include parsers.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/parsers.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include extension.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/extension.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include sha-1.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/sha-1.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include server.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/server.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include wv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/wv.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include browserMessage.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/browserMessage.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include fwv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fwv.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libwsserver.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libwsserver.a
(cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/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 \
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fwv.o; )
ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libwsserver.a
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -DSTANDALONE server.c \
-I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/servertest.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/server /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/servertest.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libwsserver.a \
-lpthread -lz -lm
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libwsserver.dylib
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libwsserver.dylib
(cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj; clang++ -g -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libwsserver.dylib \
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 \
-install_name '@rpath/libwsserver.dylib' \
-compatibility_version 7.7 \
-current_version 1.0.26 )
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/EGADS/trunk/lite
++ make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/liteBase.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteMemory.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/liteMemory.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteGeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/liteGeom.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteTopo.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/liteTopo.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteAttrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/liteAttrs.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteImport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/liteImport.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteString.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/liteString.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
../src/egadsTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/liteTess.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
../src/egadsTris.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/liteTris.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src \
../src/egadsQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/liteQuads.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
-I../util ../src/egadsTessInp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/liteTessInp.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
../util/evaluate.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/evaLite.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE ../util/rational.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/ratLite.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I../util \
../util/regQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/liteRegQuads.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
../src/egadsEffect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/liteEffect.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
-I../util/uvmap liteUVmap.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/liteUVmap.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libegadslite.dylib
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libegadslite.dylib
(cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libegadslite.dylib \
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 \
-install_name '@rpath/libegadslite.dylib' \
-current_version 1.0.26 )
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libegadslitestatic.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libegadslitestatic.a
(cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/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 archive /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libegadslitestatic.a
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/EGADS/trunk/test
+++ ls BSplineIGES.make CSys.make GBO.make SBO.make addKnots.make agglom.make approx.make blend.make chamfer.make closure.make edge2WB.make edges.make effective.make egads2cart.make egads2ply.make egadsGeom_dot.make egadsHLevel_dot.make egadsSpline_dot.make egadsTopo_dot.make exportLite.make extrot.make fillet.make fit.make fitTri.make fullAttr.make fuseSheets.make globalTess.make hollow.make hollowFace.make intersect.make makeCone.make makeFace3D.make makeLoop.make mapTess.make mofb.make mssb.make multiContext.make offset.make rebuild.make refObj.make replace.make revolve.make ruled.make saveTess.make scribe.make sew.make simplePer.make smallEdges.make step.make sweep.make test.make tolerance.make union.make vAttr.make vCurvature.make vEffect.make vEto.make vFrame.make vGeom.make vQuad.make vTess.make vTessInp.make xform.make
++ for file in '`ls *.make`'
++ make -f BSplineIGES.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include BSplineIGES.c -o \
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/BSplineIGES.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/BSplineIGES /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/BSplineIGES.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f CSys.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include CSys.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/CSys.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/CSys /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/CSys.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f GBO.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include GBO.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/GBO.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/GBO /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/GBO.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f SBO.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include SBO.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/SBO.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/SBO /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/SBO.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f addKnots.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include addKnots.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/addKnots.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/addKnots /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/addKnots.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f agglom.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include agglom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/agglom.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/agglom /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/agglom.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -legads -lm
++ for file in '`ls *.make`'
++ make -f approx.make
gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include approx.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/approx.o
gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/approx /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/approx.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lfgads \
-legads -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -Wl,-w
++ for file in '`ls *.make`'
++ make -f blend.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include blend.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/blend.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/blend /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/blend.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f chamfer.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include chamfer.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/chamfer.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/chamfer /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/chamfer.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f closure.make
gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include closure.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/closure.o
gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/closure /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/closure.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lfgads \
-legads -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -Wl,-w
++ for file in '`ls *.make`'
++ make -f edge2WB.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include edge2WB.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/edge2WB.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/edge2WB /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/edge2WB.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f edges.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include edges.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/edges.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/edges /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/edges.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f effective.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include effective.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/effective.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/effective /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/effective.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f egads2cart.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include egads2cart.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads2cart.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/egads2cart /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads2cart.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f egads2ply.make
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. egads2ply.cpp -std=c++11 \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads2ply.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -I. tinyply.cpp -std=c++11 -w \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/tinyply.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/egads2ply /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads2ply.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/tinyply.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f egadsGeom_dot.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include egadsGeom_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsGeom_dot.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include egadsTools_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsTools_dot.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/egadsGeom_dot /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsGeom_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f egadsHLevel_dot.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include egadsHLevel_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsHLevel_dot.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/egadsHLevel_dot /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsHLevel_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f egadsSpline_dot.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include egadsSpline_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsSpline_dot.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/egadsSpline_dot /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsSpline_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f egadsTopo_dot.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include egadsTopo_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsTopo_dot.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/egadsTopo_dot /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsTopo_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f exportLite.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../util/uvmap \
../src/egadsExport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/exportLite.o -DSTANDALONE
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/exportLite /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/exportLite.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f extrot.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include extrot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/extrot.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/extrot /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/extrot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f fillet.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include fillet.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fillet.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/fillet /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fillet.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f fit.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include fit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fit.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/fit /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fit.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f fitTri.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include fitTri.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fitTri.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/fitTri /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fitTri.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f fullAttr.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include fullAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fullAttr.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/fullAttr /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fullAttr.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f fuseSheets.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include fuseSheets.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fuseSheets.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/fuseSheets /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fuseSheets.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f globalTess.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include globalTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/globalTess.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/globalTess /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/globalTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f hollow.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include hollow.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hollow.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/hollow /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hollow.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f hollowFace.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include hollowFace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hollowFace.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/hollowFace /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hollowFace.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f intersect.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include intersect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/intersect.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/intersect /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/intersect.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f makeCone.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include makeCone.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/makeCone.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/makeCone /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/makeCone.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f makeFace3D.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include makeFace3D.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/makeFace3D.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/makeFace3D /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/makeFace3D.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f makeLoop.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include makeLoop.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/makeLoop.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/makeLoop /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/makeLoop.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f mapTess.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include mapTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/mapTess.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/mapTess /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/mapTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f mofb.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include mofb.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/mofb.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/mofb /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/mofb.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f mssb.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include mssb.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/mssb.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/mssb /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/mssb.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f multiContext.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include multiContext.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/multiContext.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/multiContext /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/multiContext.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib \
-legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f offset.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include offset.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/offset.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/offset /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/offset.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f rebuild.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include rebuild.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/rebuild.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/rebuild /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/rebuild.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f refObj.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include refObj.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/refObj.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/refObj /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/refObj.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f replace.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include replace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/replace.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/replace /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/replace.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f revolve.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include revolve.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/revolve.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/revolve /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/revolve.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f ruled.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include ruled.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/ruled.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/ruled /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/ruled.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f saveTess.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include saveTess.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/saveTess.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/saveTess /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/saveTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f scribe.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include scribe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/scribe.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/scribe /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/scribe.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f sew.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include sew.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/sew.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/sew /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/sew.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f simplePer.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include simplePer.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/simplePer.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/simplePer /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/simplePer.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f smallEdges.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include smallEdges.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/smallEdges.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/smallEdges /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/smallEdges.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f step.make
gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include step.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/step.o
gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/step /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/step.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lfgads -legads \
-Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -Wl,-w
++ for file in '`ls *.make`'
++ make -f sweep.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include sweep.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/sweep.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/sweep /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/sweep.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f test.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include testc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/testc.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/testc /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/testc.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include testf.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/testf.o
gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/testf /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/testf.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lfgads -legads \
-Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -Wl,-w
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include parsec.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/parsec.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/parsec /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/parsec.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include parsef.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/parsef.o
gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/parsef /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/parsef.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lfgads -legads \
-Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -Wl,-w
++ for file in '`ls *.make`'
++ make -f tolerance.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include tolerance.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/tolerance.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/tolerance /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/tolerance.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ for file in '`ls *.make`'
++ make -f union.make
gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include union.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/union.o
gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/union /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/union.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lfgads -legads \
-Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -Wl,-w
++ for file in '`ls *.make`'
++ make -f vAttr.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include vAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vAttr.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/vAttr /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vAttr.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
++ for file in '`ls *.make`'
++ make -f vCurvature.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include vCurvature.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vCurvature.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/vCurvature /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vCurvature.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
++ for file in '`ls *.make`'
++ make -f vEffect.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include vEffect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vEffect.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/vEffect /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vEffect.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
++ for file in '`ls *.make`'
++ make -f vEto.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include vEto.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vEto.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/vEto /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vEto.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
++ for file in '`ls *.make`'
++ make -f vFrame.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include vFrame.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vFrame.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/vFrame /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vFrame.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
++ for file in '`ls *.make`'
++ make -f vGeom.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include vGeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vGeom.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/vGeom /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vGeom.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
++ for file in '`ls *.make`'
++ make -f vQuad.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include vQuad.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vQuad.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/vQuad /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vQuad.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lwsserver \
-legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
++ for file in '`ls *.make`'
++ make -f vTess.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include vTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vTess.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include ../util/retessFaces.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/retessFaces.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/vTesstatic /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vTess.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/retessFaces.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lwsserver -legadstatic -L/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet \
-lpthread -lz -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/vTess /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vTess.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/retessFaces.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
++ for file in '`ls *.make`'
++ make -f vTessInp.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include vTessInp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vTessInp.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/vTessInp /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vTessInp.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
++ for file in '`ls *.make`'
++ make -f xform.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include xform.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/xform.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/xform /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/xform.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/EGADS/trunk/docs/Tutorial
++ make -f tire.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include tire.c
clang++ -g -o tire tire.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ make -f egads2tri.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include egads2tri.c
clang++ -g -o egads2tri egads2tri.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/EGADS/trunk/docs/EGADS_dot/src
++ make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. circle1_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/circle1_dot.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. pingBodies.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/pingBodies.o
clang -g -o circle1_dot /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/circle1_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/pingBodies.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. circle2_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/circle2_dot.o
clang -g -o circle2_dot /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/circle2_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/pingBodies.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. naca_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/naca_dot.o
clang -g -o naca_dot /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/naca_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/pingBodies.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. ruled_naca_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/ruled_naca_dot.o
clang -g -o ruled_naca_dot /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/ruled_naca_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/pingBodies.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/OpenCSM/trunk/src
++ make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. serveCSM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/serveCSM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. OpenCSM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/OpenCSM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udp.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. tim.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/tim.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libocsm.dylib
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libocsm.dylib
clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libocsm.dylib /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/OpenCSM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udp.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/tim.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -lwsserver -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -install_name '@rpath/libocsm.dylib' -compatibility_version 1.0.26 -current_version 1.0.26
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/serveCSM /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/serveCSM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. serveESP.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/serveESP.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/serveESP /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/serveESP.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. sensCSM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/sensCSM.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/sensCSM /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/sensCSM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpBezier.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpBezier.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/bezier.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/bezier.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/bezier.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpBezier.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpBiconvex.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpBiconvex.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/biconvex.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/biconvex.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/biconvex.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpBiconvex.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpBox.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpBox.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/box.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/box.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/box.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpBox.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpBspline.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpBspline.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/bspline.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/bspline.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/bspline.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpBspline.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfCatmull.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfCatmull.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/catmull.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/catmull.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/catmull.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfCatmull.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfCompare.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfCompare.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/compare.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/compare.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/compare.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfCompare.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfCreateBEM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfCreateBEM.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/createBEM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/createBEM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/createBEM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfCreateBEM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfCreatePoly.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfCreatePoly.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/createPoly.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/createPoly.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/createPoly.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfCreatePoly.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpCsm.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpCsm.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/csm.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/csm.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/csm.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpCsm.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfDeform.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfDeform.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/deform.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/deform.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/deform.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfDeform.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfDroop.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfDroop.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/droop.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/droop.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/droop.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfDroop.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfDumpPmtrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfDumpPmtrs.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/dumpPmtrs.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/dumpPmtrs.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/dumpPmtrs.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfDumpPmtrs.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfEditAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfEditAttr.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/editAttr.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/editAttr.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/editAttr.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfEditAttr.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpEllipse.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpEllipse.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/ellipse.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/ellipse.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/ellipse.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpEllipse.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpEqn2body.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpEqn2body.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/eqn2body.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/eqn2body.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/eqn2body.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpEqn2body.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpFitcurve.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpFitcurve.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/fitcurve.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/fitcurve.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/fitcurve.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpFitcurve.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfFlend.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfFlend.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/flend.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/flend.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/flend.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfFlend.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpFreeform.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpFreeform.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/freeform.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/freeform.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/freeform.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpFreeform.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfGanged.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfGanged.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/ganged.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/ganged.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/ganged.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfGanged.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfGuide.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfGuide.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/guide.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/guide.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/guide.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfGuide.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpHex.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpHex.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/hex.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/hex.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/hex.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpHex.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpImport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpImport.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/import.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/import.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/import.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpImport.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpKulfan.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpKulfan.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/kulfan.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/kulfan.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/kulfan.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpKulfan.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfLinalg.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfLinalg.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/linalg.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/linalg.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/linalg.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfLinalg.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfMatchBodys.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfMatchBodys.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/matchBodys.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/matchBodys.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/matchBodys.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfMatchBodys.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfMechanism.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfMechanism.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/mechanism.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/mechanism.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/mechanism.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfMechanism.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpNaca.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpNaca.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/naca.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/naca.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/naca.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpNaca.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfNaca6mc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfNaca6mc.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/naca6mc.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/naca6mc.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/naca6mc.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfNaca6mc.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfNacelle.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfNacelle.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/nacelle.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/nacelle.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/nacelle.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfNacelle.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpNurbbody.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpNurbbody.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/nurbbody.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/nurbbody.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/nurbbody.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpNurbbody.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfNuscale.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfNuscale.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/nuscale.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/nuscale.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/nuscale.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfNuscale.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfOffset.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfOffset.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/offset.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/offset.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/offset.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfOffset.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpParabaloid.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpParabaloid.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/parabaloid.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/parabaloid.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/parabaloid.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpParabaloid.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpParsec.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpParsec.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/parsec.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/parsec.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/parsec.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpParsec.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpPod.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpPod.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/pod.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/pod.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/pod.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpPod.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpPoly.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpPoly.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/poly.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/poly.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/poly.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpPoly.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfPrintBbox.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfPrintBbox.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/printBbox.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/printBbox.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/printBbox.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfPrintBbox.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfPrintBrep.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfPrintBrep.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/printBrep.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/printBrep.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/printBrep.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfPrintBrep.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfPrintEgo.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfPrintEgo.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/printEgo.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/printEgo.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/printEgo.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfPrintEgo.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpProp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpProp.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/prop.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/prop.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/prop.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpProp.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpRadwaf.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpRadwaf.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/radwaf.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/radwaf.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/radwaf.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpRadwaf.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpSample.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpSample.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/sample.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/sample.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/sample.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpSample.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpSew.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpSew.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/sew.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/sew.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/sew.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpSew.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfShadow.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfShadow.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/shadow.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/shadow.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/shadow.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfShadow.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfSlices.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfSlices.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/slices.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/slices.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/slices.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfSlices.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpStag.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpStag.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/stag.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/stag.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/stag.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpStag.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfStiffener.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfStiffener.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/stiffener.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/stiffener.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/stiffener.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfStiffener.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpSupell.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpSupell.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/supell.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/supell.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/supell.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpSupell.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfTester1.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfTester1.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/tester1.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/tester1.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/tester1.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfTester1.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpTester2.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpTester2.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/tester2.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/tester2.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/tester2.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpTester2.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpVsp3.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpVsp3.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/vsp3.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/vsp3.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/vsp3.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpVsp3.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpWaffle.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpWaffle.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/waffle.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/waffle.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/waffle.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpWaffle.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udfWarp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfWarp.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/warp.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/warp.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/warp.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udfWarp.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. eggPDT2.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/eggPDT2.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/PDT2.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/PDT2.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/PDT2.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/eggPDT2.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. udpNaca456.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpNaca456.o
gfortran -g -c -O -frecursive -fcray-pointer naca456.f90 -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/naca456.o -J /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/naca456.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/naca456.so
gfortran -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/naca456.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/udpNaca456.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/naca456.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm -Wl,-w
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. timEreped.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timEreped.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/ereped.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/ereped.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/ereped.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timEreped.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. timMitten.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timMitten.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/mitten.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/mitten.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/mitten.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timMitten.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. timPlotter.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timPlotter.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/plotter.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/plotter.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/plotter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timPlotter.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. timPlugs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timPlugs.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/plugs.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/plugs.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/plugs.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timPlugs.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. timSlugs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timSlugs.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/slugs.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/slugs.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/slugs.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timSlugs.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. timVspSetup.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timVspSetup.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/vspSetup.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/vspSetup.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/vspSetup.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timVspSetup.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -lm
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/OpenCSM.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/OpenCSM.h
cp -p OpenCSM.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/OpenCSM.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/common.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/common.h
cp -p common.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/common.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/udp.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/udp.h
cp -p udp.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/udp.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/esp.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/esp.h
cp -p esp.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/esp.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/tim.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/tim.h
cp -p tim.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/tim.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egg.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egg.h
cp -p egg.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/egg.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/udpUtilities.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/udpUtilities.h
cp -p udpUtilities.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/udpUtilities.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/udpUtilities.c
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/udpUtilities.c
cp -p udpUtilities.c /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/udpUtilities.c
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/EGADS/trunk/docs/UDP_UDF/data
++ make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include udpTire.c -o tire.o
clang -g -o tire tire.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DUDP -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include udpTire.c
touch tire.so
rm tire.so
clang -g -bundle -o tire.so udpTire.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
++ [[ '' == '' ]]
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS
++ make
(cd src; make)
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/caps.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/caps.h
cp -p ../include/caps.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/caps.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/capsErrors.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/capsErrors.h
cp -p ../include/capsErrors.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/capsErrors.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/capsTypes.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/capsTypes.h
cp -p ../include/capsTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/capsTypes.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aimUtil.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aimUtil.h
cp -p ../include/aimUtil.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aimUtil.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aimMesh.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aimMesh.h
cp -p ../include/aimMesh.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aimMesh.h
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../include \
-I/usr/include/udunits2 aimUtil.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aimUtil.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include \
-I/usr/include/udunits2 aimTransferUtil.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aimTransferUtil.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../include \
aimMesh.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aimMesh.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libaimUtil.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libaimUtil.a
ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libaimUtil.a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aimUtil.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aimMesh.o \
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aimTransferUtil.o
ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libaimUtil.a
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. \
-I/usr/include/udunits2 capsBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/capsBase.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. \
-I/usr/include/udunits2 capsAnalysis.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/capsAnalysis.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. \
-I/usr/include/udunits2 capsApprox.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/capsApprox.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. \
-I/usr/include/udunits2 capsAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/capsAttr.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. \
-I/usr/include/udunits2 capsAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/capsAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. \
-I/usr/include/udunits2 capsBound.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/capsBound.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. \
-I/usr/include/udunits2 capsProblem.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/capsProblem.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. \
-I/usr/include/udunits2 capsValue.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/capsValue.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. \
-I/usr/include/udunits2 capsUnits.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/capsUnits.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. \
-I/usr/include/udunits2 conjGrad.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/conjGrad.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. \
-I/usr/include/udunits2 capsFunIDs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/capsFunIDs.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. \
-I/usr/include/udunits2 capsChkInpt.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/capsChkInpt.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. \
-I/usr/include/udunits2 printObject.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/printObject.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libcaps.dylib
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libcaps.dylib
(cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libcaps.dylib 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 \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -ludunits2 -locsm -legads -ldl \
-install_name '@rpath/libcaps.dylib' \
-compatibility_version 1.0.26 \
-current_version 1.0.26 )
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libcapsstatic.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libcapsstatic.a
(cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj; ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/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 archive /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libcapsstatic.a
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include testingAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/testingAIM.o
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/testingAIM.so
rm: /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/testingAIM.so: No such file or directory
make[1]: [/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/testingAIM.so] Error 1 (ignored)
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/testingAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/testingAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include testingWriter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/testingWriter.o
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/testingWriter.so
rm: /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/testingWriter.so: No such file or directory
make[1]: [/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/testingWriter.so] Error 1 (ignored)
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/testingWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/testingWriter.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -laimUtil -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include phaseUtil.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/phaseUtil.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/phaseUtil /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/phaseUtil.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -ludunits2 -locsm -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
(cd aim; make)
/Library/Developer/CommandLineTools/usr/bin/make -C utils
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython attrUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/attrUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython meshUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/meshUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cfdUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/cfdUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython miscUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/miscUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython feaUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/feaUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython vlmUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vlmUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranCards.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/nastranCards.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/nastranUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython tecplotUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/tecplotUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython arrayUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/arrayUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython deprecateUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/deprecateUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cardUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/cardUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython jsonUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/jsonUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cython/nastranOP2Reader.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/nastranOP2Reader.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. vlmSpanSpace.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vlmSpanSpace.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libutils.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libutils.a
(cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj; ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/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 archive /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libutils.a
/Library/Developer/CommandLineTools/usr/bin/ranlib: file: /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libutils.a(attrUtils.o) has no symbols
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils
cp -p -f arrayUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/arrayUtils.h
cp -p -f attrTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/attrTypes.h
cp -p -f attrUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/attrUtils.h
cp -p -f cardTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/cardTypes.h
cp -p -f cardUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/cardUtils.h
cp -p -f cfdTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/cfdTypes.h
cp -p -f cfdUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/cfdUtils.h
cp -p -f deprecateUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/deprecateUtils.h
cp -p -f feaTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/feaTypes.h
cp -p -f feaUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/feaUtils.h
cp -p -f jsonUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/jsonUtils.h
cp -p -f meshTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/meshTypes.h
cp -p -f meshUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/meshUtils.h
cp -p -f miscTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/miscTypes.h
cp -p -f miscUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/miscUtils.h
cp -p -f nastranCards.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/nastranCards.h
cp -p -f nastranUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/nastranUtils.h
cp -p -f tecplotUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/tecplotUtils.h
cp -p -f vlmSpanSpace.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/vlmSpanSpace.h
cp -p -f vlmTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/vlmTypes.h
cp -p -f vlmUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/aim/utils/vlmUtils.h
/Library/Developer/CommandLineTools/usr/bin/make -C abaqus
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils \
abaqusAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/abaqusAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils \
abaqusUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/abaqusUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils \
-I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/abaqusFILReader.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/abaqusFILReader.o
echo "Building Abaqus with Python"
Building Abaqus with Python
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/abaqusAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/abaqusAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/abaqusUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/abaqusFILReader.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w -lm -ldl -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
/Library/Developer/CommandLineTools/usr/bin/make -C aflr2
clang -g -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src aflr2_version.c \
-L/Users/jenkins/util/AFLR/aflr_lib_11.5.15/MacOSX-x86-64/lib -laflr2c -lm \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr2_version
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr2_version
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src \
-I../utils aflr2AIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr2AIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src \
-I../utils aflr2_Interface.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr2_Interface.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/aflr2AIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/aflr2AIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/aflr2AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr2AIM.o \
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr2_Interface.o -L/Users/jenkins/util/AFLR/aflr_lib_11.5.15/MacOSX-x86-64/lib \
-laflr2c -legen -lrec2 -ldftr2 -ldftr3 -ldgeom -lotb -lqtb -lug_io -lug_cpp -lice2 -lug3 -lug2 -lug_gq -lug -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils \
-laimUtil -locsm -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -lm
/Library/Developer/CommandLineTools/usr/bin/make -C aflr3
clang -g -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src aflr3_version.c \
-L/Users/jenkins/util/AFLR/aflr_lib_11.5.15/MacOSX-x86-64/lib -laflr3 \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr3_version
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr3_version
16.32.50
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src \
aflr3AIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr3AIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src \
aflr3_Interface.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr3_Interface.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/EG_getEffBodyTopos.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/EG_getEffBodyTopos.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_aflr4_check_tess_coord.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_check_tess_coord.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_aflr4_check_tess_ordering.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_check_tess_ordering.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_aflr4_get_bedge_coord.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_bedge_coord.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_aflr4_get_edge_spacing.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_edge_spacing.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_aflr4_get_faceOrder.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_faceOrder.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_aflr4_get_face_spacing.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_face_spacing.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_aflr4_get_surf_grid.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_surf_grid.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_aflr4_create_tess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_create_tess.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_aflr4_tess_to_dgeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_tess_to_dgeom.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_aflr4_version.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_version.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_auto_cad_geom_setup.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_auto_cad_geom_setup.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_add_attr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_attr.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_add_ff.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_ff.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_add_ret_attr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_ret_attr.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_bodyFlag.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_bodyFlag.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_check_bc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_check_bc.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_data_cleanup.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_data_cleanup.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_edgeData.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edgeData.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_edgeFace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edgeFace.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_edit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edit.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_faceEdge.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceEdge.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_faceFace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceFace.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_faceFlag.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceFlag.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_faceLoop.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceLoop.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_file_read.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_file_read.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_file_write.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_file_write.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_idef2idef.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_idef2idef.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_loopEdge.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_loopEdge.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_nodeData.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_nodeData.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_reset_attr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_reset_attr.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_setup.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_setup.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_write_topo_data.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_write_topo_data.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_eval_curv_at_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_curv_at_uv.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_eval_edge_arclen.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_edge_arclen.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_eval_norm_at_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_norm_at_uv.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_eval_uv_at_t.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_at_t.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_eval_uv_at_xyz.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_at_xyz.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_eval_uv_bounds.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_bounds.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_eval_xyz_at_u.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_xyz_at_u.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_eval_xyz_at_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_xyz_at_uv.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_face_node_map.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_face_node_map.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_cad_geom_faceMatch.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceMatch.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_data.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_data.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src /Users/jenkins/util/AFLR/aflr_lib_11.5.15/src/egads_aflr4/egads_mzone.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_mzone.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/aflr3AIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/aflr3AIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/aflr3AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr3AIM.o \
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr3_Interface.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/EG_getEffBodyTopos.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_check_tess_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_check_tess_ordering.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_bedge_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_edge_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_faceOrder.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_face_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_surf_grid.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_create_tess.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_tess_to_dgeom.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_version.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_auto_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_ff.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_ret_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_bodyFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_check_bc.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_data_cleanup.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edgeData.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edgeFace.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edit.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceFace.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceLoop.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_file_read.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_file_write.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_idef2idef.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_loopEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_nodeData.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_reset_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_write_topo_data.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_curv_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_edge_arclen.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_norm_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_at_t.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_at_xyz.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_bounds.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_xyz_at_u.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_xyz_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_face_node_map.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceMatch.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_data.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_mzone.o -L/Users/jenkins/util/AFLR/aflr_lib_11.5.15/MacOSX-x86-64/lib \
-laflr3 -laflr43 -laflr4 -lsurf_auto_cpp -lsurf_auto -lrec3 -lug_mp -lanbl3 -laflr2c -lrec2 -lbl1 -lotb -legen -lice2 -lice3 -ldftr2 -ldftr3 -ldgeom -lug_io -lug_gq -lug_cpp -lcgns -lqtb -lug3 -lug -lug2 -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils \
-laimUtil -locsm -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -lm
/Library/Developer/CommandLineTools/usr/bin/make -C aflr4
clang -g -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src aflr4_version.c \
-L/Users/jenkins/util/AFLR/aflr_lib_11.5.15/MacOSX-x86-64/lib -laflr4 -lm \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr4_version
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr4_version
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src -I../utils aflr4AIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr4AIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.15/src \
-I../utils aflr4_Interface.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr4_Interface.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/aflr4AIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/aflr4AIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/aflr4AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr4AIM.o \
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr4_Interface.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/EG_getEffBodyTopos.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_check_tess_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_check_tess_ordering.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_bedge_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_edge_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_faceOrder.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_face_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_surf_grid.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_create_tess.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_tess_to_dgeom.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_version.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_auto_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_ff.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_ret_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_bodyFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_check_bc.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_data_cleanup.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edgeData.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edgeFace.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edit.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceFace.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceLoop.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_file_read.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_file_write.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_idef2idef.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_loopEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_nodeData.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_reset_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_write_topo_data.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_curv_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_edge_arclen.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_norm_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_at_t.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_at_xyz.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_bounds.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_xyz_at_u.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_eval_xyz_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_face_node_map.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceMatch.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_data.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads_mzone.o -L/Users/jenkins/util/AFLR/aflr_lib_11.5.15/MacOSX-x86-64/lib \
-laflr4 -laflr2c -lsurf_auto -lsurf_auto_cpp -laflr3 -legen -lrec2 -lrec3 -ldftr3 -ldftr2 -ldgeom -lotb -lqtb -lice2 -lice3 -lug3 -lug2 -lug -lug_mp -lug_gq -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils \
-laimUtil -locsm -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -lm
/Library/Developer/CommandLineTools/usr/bin/make -C astros
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils astrosAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/astrosAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils astrosUtils.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/astrosUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils astrosCards.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/astrosCards.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/astrosAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/astrosAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/astrosUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/astrosCards.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C avl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils avlAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_BODY.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_CNC.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_CPOML.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_DERMATB.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_DERMATM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_DERMATS.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_ELE.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_HINGE.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_STRP.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_SURF.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_TOT.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_VM.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/avlAIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/avlAIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/avlAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_BODY.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_CNC.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_CPOML.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_DERMATB.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_DERMATM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_DERMATS.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_ELE.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_HINGE.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_STRP.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_SURF.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_TOT.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlRead_VM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \
-lc++ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C awave
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils awaveAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/awaveAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/awaveAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/awaveAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
gfortran -g -c -O -frecursive -fcray-pointer -std=legacy awavemod.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/awave.o
gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/awave /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/awave.o -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C cart3d
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DCAPS_MESHUTILS -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/libCart3D -I./xddm \
cart3dAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/cart3dAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/c3dio \
-I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/libCart3D -I./xddm \
writeTrix.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/writeTrix.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/c3dio \
-I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/libCart3D \
surfTrix.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/surfTrix.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -pedantic -I./xddm -I. \
`xml2-config --cflags` ./xddm/xddm.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/xddm.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include bodyTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/bodyTess.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/cart3dAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/cart3dAIM.o \
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/writeTrix.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/surfTrix.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/xddm.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/bodyTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils \
-laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/ \
-lc3dio -lCart3D -ldl -lxml2 -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include cart3dTest.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/cart3dTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/cart3dTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/cart3dTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I./xddm \
-I. `xml2-config --cflags` ESPxddm.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/ESPxddm.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/ESPxddm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/ESPxddm.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/writeTrix.o \
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/surfTrix.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/xddm.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/bodyTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -locsm -legads \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include/ -lc3dio -lCart3D \
-lpthread -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lxml2 -lm
/Library/Developer/CommandLineTools/usr/bin/make -C cbaero
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/cbaeroAIM.o
clang -g -bundle /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/cbaeroAIM.o -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/cbaeroAIM.so -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
/Library/Developer/CommandLineTools/usr/bin/make -C cgt
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include egads2cgt.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads2cgt.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include aflr4egads.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr4egads.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/egads2cgt /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egads2cgt.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aflr4egads.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads -lcaps -locsm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
/Library/Developer/CommandLineTools/usr/bin/make -C custom
make[2]: Nothing to be done for `default'.
/Library/Developer/CommandLineTools/usr/bin/make -C delaundo
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils delaundoAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/delaundoAIM.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/delaundoAIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/delaundoAIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/delaundoAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/delaundoAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C egadsTess
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils egadsTessAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsTessAIM.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/egadsTessAIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/egadsTessAIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/egadsTessAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/egadsTessAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C friction
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -Wno-format -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils frictionAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/frictionAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/frictionAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/frictionAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
gfortran -g -c -O -frecursive -fcray-pointer friction_eja_mod.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/friction.o
gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/friction /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/friction.o -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C fun3d
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils -I../meshWriter/ugridWriter \
-I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython fun3dAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fun3dAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils -I../meshWriter/ugridWriter \
fun3dUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fun3dUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils \
-I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/fun3dNamelist.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fun3dNamelist.o
Building FUN3D with Python
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/fun3dAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fun3dAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fun3dUtils.o \
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fun3dNamelist.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -ldl -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w -lm -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
/Library/Developer/CommandLineTools/usr/bin/make -C hsm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils hsmAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils hsmUtils.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils hsmAdj.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmAdj.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -Wno-comment rcm/rcm.cpp -DREVISION=7.7 \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/rcm.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 rcm/genrcmi.cpp -DREVISION=7.7 \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/genrcmi.o
/Library/Developer/CommandLineTools/usr/bin/make -C src atanc.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero atanc.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/atanc.o
/Library/Developer/CommandLineTools/usr/bin/make -C src bmdump.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero bmdump.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/bmdump.o
/Library/Developer/CommandLineTools/usr/bin/make -C src cross.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero cross.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/cross.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmabd.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmabd.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmabd.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmbb2.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbb2.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmbb2.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmbc.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbc.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmbc.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmdep.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmdep.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmdep.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmeqn.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmeqn.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmeqn.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmgeo.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmgeo.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmgeo.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmglr.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmglr.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmglr.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmout.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmout.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmout.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmprj.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmprj.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmprj.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmre1.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmre1.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmre1.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmren.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmren.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmren.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmrfm.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmrfm.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmrfm.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmrun.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero -fno-recursive hsmrun.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmrun.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmsol.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmsol.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmsol.o
/Library/Developer/CommandLineTools/usr/bin/make -C src ludcmp.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero ludcmp.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/ludcmp.o
/Library/Developer/CommandLineTools/usr/bin/make -C src sbsolve.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero sbsolve.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/sbsolve.o
/Library/Developer/CommandLineTools/usr/bin/make -C src /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libhsm.a
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libhsm.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libhsm.a
(cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj; ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/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 archive /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libhsm.a
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/hsmAIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/hsmAIM.so
gfortran -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/hsmAIM.so \
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmAdj.o \
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/rcm.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/genrcmi.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -lhsm -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C interference
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include interferenceAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/interferenceAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. cloudFns.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/cloudFns.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/interferenceAIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/interferenceAIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/interferenceAIM.so \
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/interferenceAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/cloudFns.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib \
-laimUtil -locsm -legads -ludunits2 -ldl -lc++ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C jfd3
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils jfd3AIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/jfd3AIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/jfd3AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/jfd3AIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C masstran
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils masstranAIM.cpp \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/masstranAIM.o
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/masstranAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/masstranAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C meshWriter
/Library/Developer/CommandLineTools/usr/bin/make -C bstlWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include bstlWriter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/bstlWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/bstlWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/bstlWriter.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C bvtkWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include bvtkWriter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/bvtkWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/bvtkWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/bvtkWriter.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C exodusWriter
clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/sandialabs/seacas/include -I. exodusWriter.cpp \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/exodusWriter.o
clang++ -g -bundle -std=c++11 -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/exodusWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/exodusWriter.o \
-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C fastWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include fastWriter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fastWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/fastWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fastWriter.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C libmeshbWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include libmeshbWriter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/libmeshbWriter.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -IlibMeshb/sources -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include libMeshb/sources/libmeshb7.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/libmeshb7.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/libmeshbWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/libmeshbWriter.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/libmeshb7.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C stlWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include stlWriter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/stlWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/stlWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/stlWriter.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C su2Writer
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include su2Writer.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/su2Writer.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/su2Writer.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/su2Writer.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C tecplotWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include tecplotWriter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/tecplotWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/tecplotWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/tecplotWriter.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C ugridWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include ugridWriter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/ugridWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/ugridWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/ugridWriter.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C vtkWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include vtkWriter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vtkWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/vtkWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vtkWriter.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C mses
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils msesAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/msesAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils msesUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/msesUtils.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/msesAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/msesAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/msesUtils.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C mystran
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils mystranAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/mystranAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils mystranUtils.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/mystranUtils.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/mystranAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/mystranAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/mystranUtils.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C nastran
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils nastranAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/nastranAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/nastranAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/nastranAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C plato
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../meshWriter/exodusWriter -I../utils -I/Users/jenkins/util/sandialabs/seacas/include -I. platoAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/platoAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/platoAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/platoAIM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib \
-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \
-laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C pointwise
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils pointwiseAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/pointwiseAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils hashElement.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hashElement.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/pointwiseAIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/pointwiseAIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/pointwiseAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/pointwiseAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hashElement.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -lpthread
/Library/Developer/CommandLineTools/usr/bin/make -C refine
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils -I../meshWriter/libmeshbWriter refineAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/refineAIM.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/refineAIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/refineAIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/refineAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/refineAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/libmeshb7.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C sierraSD
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../meshWriter/exodusWriter -I../utils -I/Users/jenkins/util/sandialabs/seacas/include -I. sierraSDAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/sierraSDAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/sierraSDAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/sierraSDAIM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib \
-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \
-lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C sierraSM
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../meshWriter/exodusWriter -I../utils -I/Users/jenkins/util/sandialabs/seacas/include -I. sierraSMAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/sierraSMAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/sierraSMAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/sierraSMAIM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib \
-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \
-lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C skeleton
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils skeletonAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/skeletonAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/skeletonAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/skeletonAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C spinnaker
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include \
-I../meshWriter/exodusWriter \
-I../meshWriter/libmeshbWriter \
-I../utils -I/Users/jenkins/util/sandialabs/seacas/include \
-I. \
spinnakerAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/spinnakerAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/spinnakerAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/spinnakerAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/libmeshb7.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib \
-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \
-laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C su2
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../meshWriter/su2Writer -I../utils su2AIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/su2AIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils su2Utils.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/su2Utils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils su2_4_Cardinal.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/su2_4_Cardinal.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils su2_5_Raven.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/su2_5_Raven.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils su2_6_Falcon.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/su2_6_Falcon.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils su2_7_Blackbird.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/su2_7_Blackbird.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils su2_801_Harrier.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/su2_801_Harrier.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/su2AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/su2AIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/su2Utils.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/su2_4_Cardinal.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/su2_5_Raven.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/su2_6_Falcon.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/su2_7_Blackbird.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/su2_801_Harrier.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C tacs
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils tacsAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/tacsAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/tacsAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/tacsAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C tetgen
clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils tetgenAIM.cpp \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/tetgenAIM.o
clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/tetgen/tetgen1.6.0 -I../utils \
-DTETLIBRARY tetgen_Interface.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/tetgen_Interface.o
clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DTETLIBRARY -w /Users/jenkins/util/tetgen/tetgen1.6.0/tetgen.cxx -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/tetgen.o
clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -O0 -w /Users/jenkins/util/tetgen/tetgen1.6.0/predicates.cxx -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/predicates.o
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/tetgenAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/tetgenAIM.o \
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/tetgen_Interface.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/tetgen.o \
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/predicates.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C tsfoil
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils \
tsfoilAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/tsfoilAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/tsfoilAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/tsfoilAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C unitTest
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS
cp -p -f pyCAPS/Mesh_Formats.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/Mesh_Formats.py
cp -p -f pyCAPS/test_aflr2.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_aflr2.py
cp -p -f pyCAPS/test_aflr3.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_aflr3.py
cp -p -f pyCAPS/test_aflr4.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_aflr4.py
cp -p -f pyCAPS/test_astros.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_astros.py
cp -p -f pyCAPS/test_avl.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_avl.py
cp -p -f pyCAPS/test_cart3d.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_cart3d.py
cp -p -f pyCAPS/test_cbaero.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_cbaero.py
cp -p -f pyCAPS/test_egadsTess.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_egadsTess.py
cp -p -f pyCAPS/test_fun3d.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_fun3d.py
cp -p -f pyCAPS/test_masstran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_masstran.py
cp -p -f pyCAPS/test_mses.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_mses.py
cp -p -f pyCAPS/test_pointwise.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_pointwise.py
cp -p -f pyCAPS/test_refine.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_refine.py
cp -p -f pyCAPS/test_su2.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_su2.py
cp -p -f pyCAPS/test_tacs.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_tacs.py
cp -p -f pyCAPS/test_tetgen.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_tetgen.py
cp -p -f pyCAPS/test_xfoil.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_xfoil.py
cp -p -f pyCAPS/test_zaero.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_zaero.py
cp -p -f pyCAPS/Makefile /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/Makefile
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData
cp -p -f csmData/airfoilSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/airfoilSection.csm
cp -p -f csmData/avlSections.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/avlSections.csm
cp -p -f csmData/cfd2D.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/cfd2D.csm
cp -p -f csmData/cfdMultiBody.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/cfdMultiBody.csm
cp -p -f csmData/cfdSingleBody.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/cfdSingleBody.csm
cp -p -f csmData/cornerGeom.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/cornerGeom.csm
cp -p -f csmData/feaSimplePlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/feaSimplePlate.csm
cp -p -f csmData/feaWingBEMAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/feaWingBEMAero.csm
cp -p -f csmData/feaWingOMLAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/feaWingOMLAero.csm
cp -p -f csmData/kulfanSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/kulfanSection.csm
cp -p -f csmData/kulfanSymmetricSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/kulfanSymmetricSection.csm
cp -p -f csmData/masstran.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/masstran.csm
cp -p -f csmData/multiRegions.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/multiRegions.csm
cp -p -f csmData/parsecSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/parsecSection.csm
cp -p -f csmData/regions.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/regions.csm
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/aimUnitTest/cCAPS
/Library/Developer/CommandLineTools/usr/bin/make -C xfoil
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils \
xfoilAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/xfoilAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/xfoilAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/xfoilAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C zaero
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils zaeroAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/zaeroAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils zaeroUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/zaeroUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils zaeroLinearFlutter.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/zaeroLinearFlutter.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils zaeroTrim.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/zaeroTrim.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils zaeroTypes.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/zaeroTypes.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils zaeroCards.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/zaeroCards.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils zaeroGeneral.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/zaeroGeneral.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../utils zaeroGraphical.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/zaeroGraphical.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/zaeroAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/zaeroAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/zaeroUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/zaeroLinearFlutter.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/zaeroTrim.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/zaeroTypes.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/zaeroCards.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/zaeroGeneral.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/zaeroGraphical.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
(cd Slugs/src; make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. Slugs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/Slugs.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. Fitter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/Fitter.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. RedBlackTree.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/RedBlackTree.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. Tessellate.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/Tessellate.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/Slugs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/Slugs.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/Fitter.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/RedBlackTree.o \
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/Tessellate.o -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads \
-lpthread -lz -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. TestFit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/TestFit.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/bin/TestFit /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/TestFit.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/Fitter.o -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -legads \
-lpthread -lz -lm
(cd test; make -f aim.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include aim.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aim.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/aim /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aim.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads \
-lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
cp -p -f testingAIM.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/testingAIM.csm
(cd test; make -f autoExec.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include autoExec.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/autoExec.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/autoExec /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/autoExec.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm \
-legads -lwsserver -lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lz -lm -ldl
(cd test; make -f newPhase.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include newPhase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/newPhase.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/newPhase /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/newPhase.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib \
-lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(cd test; make -f basic.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include basic.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/basic.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/basic /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/basic.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads\
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(cd test; make -f geomIn.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include geomIn.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/geomIn.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/geomIn /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/geomIn.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads\
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(cd test; make -f utilsTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include aimTransferUtilTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aimTransferUtilTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/aimTransferUtilTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aimTransferUtilTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -laimUtil -locsm -legads \
-lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -ludunits2 -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../aim/utils miscUtilsTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/miscUtilsTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/miscUtilsTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/miscUtilsTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -laimUtil -locsm -legads \
-lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -ludunits2 -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I../aim/utils vlmUtilsTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vlmUtilsTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/vlmUtilsTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vlmUtilsTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads \
-lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -ludunits2 -lm -ldl
(cd test; make -f vVS.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include vVS.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vVS.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/vVS /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/vVS.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
(cd examples; make)
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/analysisData
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/regressionTest
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite
cp -p -f pyCAPS/abaqus_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/abaqus_AGARD445_PyTest.py
cp -p -f pyCAPS/abaqus_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/abaqus_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Astros.py
cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Nastran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Nastran.py
cp -p -f pyCAPS/aeroelasticSimple_Displacement_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Displacement_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Displacement_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Displacement_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelasticSimple_Displacement_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Displacement_SU2_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_Cart3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Iterative_Cart3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Iterative_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Iterative_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Iterative_SU2_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Pressure_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Pressure_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Pressure_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Pressure_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelasticSimple_Pressure_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Pressure_SU2_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Temperature_SU2_and_TACS.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Temperature_SU2_and_TACS.py
cp -p -f pyCAPS/aeroelastic_Iterative_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelastic_Iterative_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelastic_Iterative_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelastic_Iterative_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelastic_Iterative_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelastic_Iterative_SU2_and_Mystran.py
cp -p -f pyCAPS/aflr2_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr2_PyTest.py
cp -p -f pyCAPS/aflr4_Generic_Missile.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_Generic_Missile.py
cp -p -f pyCAPS/aflr4_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_PyTest.py
cp -p -f pyCAPS/aflr4_QuadMesh_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_QuadMesh_PyTest.py
cp -p -f pyCAPS/aflr4_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_Symmetry_PyTest.py
cp -p -f pyCAPS/aflr4_TipTreat_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_TipTreat_PyTest.py
cp -p -f pyCAPS/aflr4_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_and_Tetgen_PyTest.py
cp -p -f pyCAPS/aflr4_and_aflr3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_and_aflr3_PyTest.py
cp -p -f pyCAPS/aflr4_and_aflr3_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_and_aflr3_Symmetry_PyTest.py
cp -p -f pyCAPS/aflr4_tetgen_Regions_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_tetgen_Regions_PyTest.py
cp -p -f pyCAPS/astros_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_AGARD445_PyTest.py
cp -p -f pyCAPS/astros_Aeroelastic_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_Aeroelastic_PyTest.py
cp -p -f pyCAPS/astros_CompositeWingFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_CompositeWingFreq_PyTest.py
cp -p -f pyCAPS/astros_Composite_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_Composite_PyTest.py
cp -p -f pyCAPS/astros_Flutter_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_Flutter_15degree.py
cp -p -f pyCAPS/astros_MultipleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_MultipleLoadCase_PyTest.py
cp -p -f pyCAPS/astros_OptControl_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_OptControl_PyTest.py
cp -p -f pyCAPS/astros_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_PyTest.py
cp -p -f pyCAPS/astros_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/astros_ThreeBarFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_ThreeBarFreq_PyTest.py
cp -p -f pyCAPS/astros_ThreeBarLinkDesign_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_ThreeBarLinkDesign_PyTest.py
cp -p -f pyCAPS/astros_ThreeBarMultiLoad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_ThreeBarMultiLoad_PyTest.py
cp -p -f pyCAPS/astros_ThreeBar_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_ThreeBar_PyTest.py
cp -p -f pyCAPS/astros_Trim_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_Trim_15degree.py
cp -p -f pyCAPS/autoLink_Pytest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/autoLink_Pytest.py
cp -p -f pyCAPS/avl_AutoSpan_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/avl_AutoSpan_PyTest.py
cp -p -f pyCAPS/avl_ControlSurf_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/avl_ControlSurf_PyTest.py
cp -p -f pyCAPS/avl_DesignSweep_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/avl_DesignSweep_PyTest.py
cp -p -f pyCAPS/avl_EigenValue_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/avl_EigenValue_PyTest.py
cp -p -f pyCAPS/avl_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/avl_OpenMDAO_3_PyTest.py
cp -p -f pyCAPS/avl_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/avl_PyTest.py
cp -p -f pyCAPS/awave_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/awave_PyTest.py
cp -p -f pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py
cp -p -f pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py
cp -p -f pyCAPS/cart3d_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cart3d_PyTest.py
cp -p -f pyCAPS/cbaero_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cbaero_PyTest.py
cp -p -f pyCAPS/delaundo_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/delaundo_PyTest.py
cp -p -f pyCAPS/egadsTess_Box_Quad_Pytest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/egadsTess_Box_Quad_Pytest.py
cp -p -f pyCAPS/egadsTess_Nose_Quad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/egadsTess_Nose_Quad_PyTest.py
cp -p -f pyCAPS/egadsTess_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/egadsTess_PyTest.py
cp -p -f pyCAPS/egadsTess_Spheres_Quad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/egadsTess_Spheres_Quad_PyTest.py
cp -p -f pyCAPS/friction_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/friction_PyTest.py
cp -p -f pyCAPS/fun3d_Morph_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_Morph_PyTest.py
cp -p -f pyCAPS/fun3d_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_OpenMDAO_3_PyTest.py
cp -p -f pyCAPS/fun3d_and_AFLR2_NodeDist_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_and_AFLR2_NodeDist_PyTest.py
cp -p -f pyCAPS/fun3d_and_AFLR2_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_and_AFLR2_PyTest.py
cp -p -f pyCAPS/fun3d_and_AFLR4_AFLR3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_and_AFLR4_AFLR3_PyTest.py
cp -p -f pyCAPS/fun3d_and_Delaundo_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_and_Delaundo_PyTest.py
cp -p -f pyCAPS/fun3d_and_Tetgen_AlphaSweep_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_and_Tetgen_AlphaSweep_PyTest.py
cp -p -f pyCAPS/fun3d_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_and_Tetgen_PyTest.py
cp -p -f pyCAPS/fun3d_refine_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_refine_PyTest.py
cp -p -f pyCAPS/hsm_CantileverPlate_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/hsm_CantileverPlate_PyTest.py
cp -p -f pyCAPS/hsm_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/hsm_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/masstran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/masstran_AGARD445_PyTest.py
cp -p -f pyCAPS/masstran_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/masstran_PyTest.py
cp -p -f pyCAPS/mses_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/mses_OpenMDAO_3_PyTest.py
cp -p -f pyCAPS/mses_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/mses_PyTest.py
cp -p -f pyCAPS/mystran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/mystran_AGARD445_PyTest.py
cp -p -f pyCAPS/mystran_MultiLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/mystran_MultiLoadCase_PyTest.py
cp -p -f pyCAPS/mystran_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/mystran_PyTest.py
cp -p -f pyCAPS/mystran_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/mystran_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/nastran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_AGARD445_PyTest.py
cp -p -f pyCAPS/nastran_Aeroelastic_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_Aeroelastic_PyTest.py
cp -p -f pyCAPS/nastran_CompositeWingDesign_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_CompositeWingDesign_PyTest.py
cp -p -f pyCAPS/nastran_CompositeWingFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_CompositeWingFreq_PyTest.py
cp -p -f pyCAPS/nastran_Composite_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_Composite_PyTest.py
cp -p -f pyCAPS/nastran_Flutter_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_Flutter_15degree.py
cp -p -f pyCAPS/nastran_MultiLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_MultiLoadCase_PyTest.py
cp -p -f pyCAPS/nastran_OptimizationMultiLoad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_OptimizationMultiLoad_PyTest.py
cp -p -f pyCAPS/nastran_PlateMisc_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_PlateMisc_PyTest.py
cp -p -f pyCAPS/nastran_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_PyTest.py
cp -p -f pyCAPS/nastran_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarDesign_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_ThreeBarDesign_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_ThreeBarFreq_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarLinkDesign_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_ThreeBarLinkDesign_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarMultiLoad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_ThreeBarMultiLoad_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBar_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_ThreeBar_PyTest.py
cp -p -f pyCAPS/nastran_Trim_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_Trim_15degree.py
cp -p -f pyCAPS/plato_aflr_airfoil_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_airfoil_PyTest.py
cp -p -f pyCAPS/plato_aflr_airfoil_morph_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_airfoil_morph_PyTest.py
cp -p -f pyCAPS/plato_aflr_cyli_box_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_cyli_box_PyTest.py
cp -p -f pyCAPS/plato_aflr_table_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_table_PyTest.py
cp -p -f pyCAPS/plato_aflr_table_morph_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_table_morph_PyTest.py
cp -p -f pyCAPS/plato_aflr_tetgen_cyli_box_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_tetgen_cyli_box_PyTest.py
cp -p -f pyCAPS/plato_aflr_tetgen_table_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_tetgen_table_PyTest.py
cp -p -f pyCAPS/plato_tetgen_cyli_box_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_tetgen_cyli_box_PyTest.py
cp -p -f pyCAPS/plato_tetgen_table_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_tetgen_table_PyTest.py
cp -p -f pyCAPS/pointwise_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/pointwise_PyTest.py
cp -p -f pyCAPS/pointwise_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/pointwise_Symmetry_PyTest.py
cp -p -f pyCAPS/su2_Morph_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_Morph_PyTest.py
cp -p -f pyCAPS/su2_X43a_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_X43a_PyTest.py
cp -p -f pyCAPS/su2_and_AFLR2_NodeDist_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_AFLR2_NodeDist_PyTest.py
cp -p -f pyCAPS/su2_and_AFLR2_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_AFLR2_PyTest.py
cp -p -f pyCAPS/su2_and_AFLR4_AFLR3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_AFLR4_AFLR3_PyTest.py
cp -p -f pyCAPS/su2_and_Delaundo_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_Delaundo_PyTest.py
cp -p -f pyCAPS/su2_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_Tetgen_PyTest.py
cp -p -f pyCAPS/su2_and_pointwise_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_pointwise_PyTest.py
cp -p -f pyCAPS/tetgen_Holes_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/tetgen_Holes_PyTest.py
cp -p -f pyCAPS/tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/tetgen_PyTest.py
cp -p -f pyCAPS/tetgen_Regions_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/tetgen_Regions_PyTest.py
cp -p -f pyCAPS/tsfoil_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/tsfoil_PyTest.py
cp -p -f pyCAPS/xfoil_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/pyCAPS/xfoil_PyTest.py
cp -p -f csmData/15degreeWing.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/15degreeWing.csm
cp -p -f csmData/aeroelasticDataTransfer.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/aeroelasticDataTransfer.csm
cp -p -f csmData/aeroelasticDataTransferSimple.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/aeroelasticDataTransferSimple.csm
cp -p -f csmData/airfoilSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/airfoilSection.csm
cp -p -f csmData/avlWing.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/avlWing.csm
cp -p -f csmData/avlWingTail.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/avlWingTail.csm
cp -p -f csmData/avlWings.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/avlWings.csm
cp -p -f csmData/awaveWingTailFuselage.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/awaveWingTailFuselage.csm
cp -p -f csmData/cfd2D.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/cfd2D.csm
cp -p -f csmData/cfd2DArbShape.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/cfd2DArbShape.csm
cp -p -f csmData/cfdMultiBody.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/cfdMultiBody.csm
cp -p -f csmData/cfdSymmetry.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/cfdSymmetry.csm
cp -p -f csmData/cfdX43a.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/cfdX43a.csm
cp -p -f csmData/cfd_airfoilSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/cfd_airfoilSection.csm
cp -p -f csmData/compositeWing.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/compositeWing.csm
cp -p -f csmData/cyli_box_shell.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/cyli_box_shell.csm
cp -p -f csmData/cyli_box_solid.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/cyli_box_solid.csm
cp -p -f csmData/feaAGARD445.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/feaAGARD445.csm
cp -p -f csmData/feaBoxes.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/feaBoxes.csm
cp -p -f csmData/feaCantileverPlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/feaCantileverPlate.csm
cp -p -f csmData/feaJoinedPlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/feaJoinedPlate.csm
cp -p -f csmData/feaSimplePlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/feaSimplePlate.csm
cp -p -f csmData/feaThreeBar.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/feaThreeBar.csm
cp -p -f csmData/feaWingBEM.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/feaWingBEM.csm
cp -p -f csmData/feaWingBEMAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/feaWingBEMAero.csm
cp -p -f csmData/frictionWingTailFuselage.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/frictionWingTailFuselage.csm
cp -p -f csmData/generic_missile.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/generic_missile.csm
cp -p -f csmData/interference.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/interference.csm
cp -p -f csmData/linearAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/linearAero.csm
cp -p -f csmData/nosecone1.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/nosecone1.csm
cp -p -f csmData/regions.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/regions.csm
cp -p -f csmData/simpleWingBox.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/simpleWingBox.csm
cp -p -f csmData/spheres.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/spheres.csm
cp -p -f csmData/table.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/table.csm
cp -p -f csmData/tiptreat.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/tiptreat.csm
cp -p -f csmData/avlWing.udc /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/csmData/avlWing.udc
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran
cp -p -f analysisData/nastran/NastranAeroWingBEM.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranAeroWingBEM.f06
cp -p -f analysisData/nastran/NastranCompositePlate.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranCompositePlate.f06
cp -p -f analysisData/nastran/NastranCompositeWing_Design.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranCompositeWing_Design.f06
cp -p -f analysisData/nastran/NastranCompositeWing_Freq.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranCompositeWing_Freq.f06
cp -p -f analysisData/nastran/NastranFlutter15Deg.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranFlutter15Deg.f06
cp -p -f analysisData/nastran/NastranMiscLoadPlate.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranMiscLoadPlate.f06
cp -p -f analysisData/nastran/NastranModalAGARD445.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranModalAGARD445.f06
cp -p -f analysisData/nastran/NastranMultiLoadPlate.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranMultiLoadPlate.f06
cp -p -f analysisData/nastran/NastranOptMultiLoadPlate.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranOptMultiLoadPlate.f06
cp -p -f analysisData/nastran/NastranSingleLoadPlate.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranSingleLoadPlate.f06
cp -p -f analysisData/nastran/NastranThreeBar.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranThreeBar.f06
cp -p -f analysisData/nastran/NastranThreeBarDesign.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranThreeBarDesign.f06
cp -p -f analysisData/nastran/NastranThreeBarFreq.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranThreeBarFreq.f06
cp -p -f analysisData/nastran/NastranThreeBarLinkDesign.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranThreeBarLinkDesign.f06
cp -p -f analysisData/nastran/NastranThreeBarMultiLoad.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranThreeBarMultiLoad.f06
cp -p -f analysisData/nastran/NastranTrim15Deg.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranTrim15Deg.f06
cp -p -f analysisData/nastran/NastranWingBEM.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranWingBEM.f06
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/csm
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/pyCAPS
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/csm
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS
cp -p -f corsairlite/boydBox.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/boydBox.py
cp -p -f corsairlite/gp.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/gp.py
cp -p -f corsairlite/hoburg_blackbox.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/hoburg_blackbox.py
cp -p -f corsairlite/hoburg_gp.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/hoburg_gp.py
cp -p -f corsairlite/qp.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/qp.py
cp -p -f corsairlite/sp.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/sp.py
cp -p -f corsairlite/capsPhase/csm/wing1.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/csm/wing1.csm
cp -p -f corsairlite/capsPhase/csm/wing2.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/csm/wing2.csm
cp -p -f corsairlite/capsPhase/pyCAPS/optTaperAvl.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/pyCAPS/optTaperAvl.py
cp -p -f corsairlite/capsPhase/pyCAPS/optWingAvl.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/pyCAPS/optWingAvl.py
cp -p -f corsairlite/capsPhase/pyCAPS/sizeWing.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/pyCAPS/sizeWing.py
cp -p -f corsairlite/multifidelity/csm/naca.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/csm/naca.csm
cp -p -f corsairlite/multifidelity/pyCAPS/CMConstraint.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/CMConstraint.py
cp -p -f corsairlite/multifidelity/pyCAPS/Camber.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/Camber.py
cp -p -f corsairlite/multifidelity/pyCAPS/FlowTrip.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/FlowTrip.py
cp -p -f corsairlite/multifidelity/pyCAPS/GPSize.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/GPSize.py
cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan2.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/Kulfan2.py
cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan4.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/Kulfan4.py
cp -p -f corsairlite/multifidelity/pyCAPS/MSES.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/MSES.py
cp -p -f corsairlite/multifidelity/pyCAPS/fullModelKulfan.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/fullModelKulfan.py
cp -p -f corsairlite/multifidelity/pyCAPS/fullModelNACA.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/fullModelNACA.py
cp -p -f regressionTest/execute_CTestRegression.sh /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/regressionTest/execute_CTestRegression.sh
cp -p -f regressionTest/execute_PyTestRegression.sh /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/regressionTest/execute_PyTestRegression.sh
(make -C cCAPS -f aeroelastic_SU2.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f avlTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include avlTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/avlTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/avlTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f awaveTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include awaveTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/awaveTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/awaveTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/awaveTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f frictionTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include frictionTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/frictionTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/frictionTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/frictionTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f fun3d.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include fun3dAFLR2Test.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fun3dAFLR2Test.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/fun3dAFLR2Test /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fun3dAFLR2Test.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include fun3dTetgenTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fun3dTetgenTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/fun3dTetgenTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/fun3dTetgenTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include aeroelasticTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aeroelasticTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/aeroelasticTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/aeroelasticTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f hsm.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include hsmTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/hsmTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include hsmSimplePlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmSimplePlateTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/hsmSimplePlateTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmSimplePlateTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include hsmCantileverPlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmCantileverPlateTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/hsmCantileverPlateTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmCantileverPlateTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include hsmJoinedPlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmJoinedPlateTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/hsmJoinedPlateTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/hsmJoinedPlateTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f interferenceTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include interferenceTest.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/interferenceTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/interferenceTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/interferenceTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f msesTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include msesTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/msesTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/msesTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/msesTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f mystran.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include mystranTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/mystranTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/mystranTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/mystranTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f pointwiseTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include pointwiseTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/pointwiseTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/pointwiseTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/pointwiseTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
+++ find /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/training/ -name Makefile
++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`'
++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/training//2023/lectures/Makefile == *\l\e\c\t\u\r\e\s* ]]
++ continue
++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`'
++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/training//2023/data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]]
+++ dirname /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/training//2023/data/session01/Makefile
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/training//2023/data/session01
++ make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include template_avl.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/template_avl.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/test/template_avl /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/template_avl.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`'
++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/training//data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]]
+++ dirname /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/training//data/session01/Makefile
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/training//data/session01
++ make
make: Nothing to be done for `default'.
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/OpenCSM/trunk/src
++ make -f serveESP.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. timCapsMode.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timCapsMode.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/capsMode.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/capsMode.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/capsMode.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timCapsMode.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. timFlowchart.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timFlowchart.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/flowchart.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/flowchart.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/flowchart.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timFlowchart.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. timViewer.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timViewer.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/viewer.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/viewer.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/viewer.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timViewer.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/include -I. -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 timPyscript.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timPyscript.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/pyscript.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/pyscript.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib/pyscript.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/obj/timPyscript.o -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
++ ln -f -s /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/OpenCSM/trunk/udc /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64
+++ find /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/OpenCSM/trunk/data/training/ -name Makefile
+ mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/test
+ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/test
+ source /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/JenkinsESP/RunRegression.sh
++ [[ 0 == 1 ]]
++ [[ 0 == 2 ]]
++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64 == '' ]]
++ [[ CAPS/AEROELASTIC == '' ]]
++ [[ 7.7 == '' ]]
++ [[ ! -d /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/JenkinsESP ]]
++ rm -f csmFiles.txt
++ [[ CAPS/AEROELASTIC =~ [0-9]+.[0-9]+ ]]
++ export ESPTEST=CAPS/AEROELASTIC
++ ESPTEST=CAPS/AEROELASTIC
++ [[ CAPS/AEROELASTIC == \C\A\P\S* ]]
++ [[ ! -d /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS ]]
++ export CAPSTARGET=AEROELASTIC
++ CAPSTARGET=AEROELASTIC
++ [[ AEROELASTIC == \u\n\i\t ]]
++ [[ AEROELASTIC == \t\r\a\i\n\i\n\g\2\0\1\8 ]]
++ [[ AEROELASTIC == \t\r\a\i\n\i\n\g ]]
++ [[ AEROELASTIC == *\_\o\f\f ]]
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/examples/
++ make test TYPE=AEROELASTIC
(make -C cCAPS -f aeroelastic_SU2.make)
make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
(make -C cCAPS -f avlTest.make)
make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/avlTest' is up to date.
(make -C cCAPS -f awaveTest.make)
make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/awaveTest' is up to date.
(make -C cCAPS -f frictionTest.make)
make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/frictionTest' is up to date.
(make -C cCAPS -f fun3d.make)
make[1]: Nothing to be done for `fun3d'.
(make -C cCAPS -f hsm.make)
make[1]: `hsm' is up to date.
(make -C cCAPS -f interferenceTest.make)
make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/interferenceTest' is up to date.
(make -C cCAPS -f msesTest.make)
make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/msesTest' is up to date.
(make -C cCAPS -f mystran.make)
make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/mystranTest' is up to date.
(make -C cCAPS -f pointwiseTest.make)
make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/cCAPS/pointwiseTest' is up to date.
(cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/regressionTest; ./execute_CTestRegression.sh AEROELASTIC)
Running.... AEROELASTIC c-Tests
All tests pass!
=================================================
=================================================
(cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/regressionTest; ./execute_PyTestRegression.sh AEROELASTIC)
=================================================
Using python : /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv/bin/python
=================================================
Running.... AEROELASTIC PyTests
=================================================
+ echo 'aeroelasticSimple_Pressure_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Pressure_SU2_and_Astros.py test;
+ python -u aeroelasticSimple_Pressure_SU2_and_Astros.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 1 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 9 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 12 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 0 1 2 3 4 5
EGADS : 2 Yes 0 0 1 0 1 1 3 5 6
EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8
EGADS : 4 Yes 0 0 1 0 1 1 3 5 6
EGADS : 5 Yes 0 0 1 0 1 1 2 4 6
EGADS : 6 Yes 0 0 1 0 1 2 3 4 5
EGADS : 7 Yes 0 0 1 0 1 3 8 9
EGADS : 8 Yes 0 0 1 0 1 3 7 9
EGADS : 9 Yes 0 0 1 0 1 7 8
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 5 6 -7 -1
EGADS : 3 -2 7 9 -8 -10 -11
EGADS : 4 -12 3 8 -13
EGADS : 5 4 12 -14 -5
EGADS : 6 -6 14 13 -9
EGADS : 7 15 10 -17 -16
EGADS : 8 17 11 -15 -18
EGADS : 9 16 18
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3 4
EGADS : 4 5
EGADS : 5 6
EGADS : 6 7
EGADS : 7 8
EGADS : 8 9
EGADS : 9 10
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes 1 2 -3 -4
EGADS : 2 Yes 5 6 -7 -1
EGADS : 3 Yes -2 7 9 -8
EGADS : 4 Yes -10 -11
EGADS : 5 Yes -12 3 8 -13
EGADS : 6 Yes 4 12 -14 -5
EGADS : 7 Yes -6 14 13 -9
EGADS : 8 Yes 15 10 -17 -16
EGADS : 9 Yes 17 11 -15 -18
EGADS : 10 Yes 16 18
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 2 1 1 1 2
EGADS : 2 0 Yes 1 3 1 1 3
EGADS : 3 0 Yes 4 3 1 1 4
EGADS : 4 0 Yes 2 4 1 1 5
EGADS : 5 0 Yes 2 5 1 2 5
EGADS : 6 0 Yes 5 6 1 2 6
EGADS : 7 0 Yes 1 6 1 2 3
EGADS : 8 0 Yes 3 7 1 3 4
EGADS : 9 0 Yes 6 7 1 3 6
EGADS : 10 0 Yes 8 9 1 3 7
EGADS : 11 0 Yes 9 8 1 3 8
EGADS : 12 0 Yes 4 10 1 4 5
EGADS : 13 0 Yes 10 7 1 4 6
EGADS : 14 0 Yes 5 10 1 5 6
EGADS : 15 0 Yes 11 8 1 7 8
EGADS : 16 0 Yes 11 12 1 7 9
EGADS : 17 0 Yes 12 9 1 7 8
EGADS : 18 0 Yes 12 11 1 8 9
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 0
EGADS : 2 Yes 0 40 0
EGADS : 3 Yes 0 0 20
EGADS : 4 Yes 0 40 20
EGADS : 5 Yes 20 40 0
EGADS : 6 Yes 20 0 0
EGADS : 7 Yes 20 0 20
EGADS : 8 Yes 1.61374306 0 0
EGADS : 9 Yes 0 0 0
EGADS : 10 Yes 20 40 20
EGADS : 11 Yes 2.53650745 3.87298335 0.334116517
EGADS : 12 Yes 1.57194608 3.87298335 0.249728332
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 40
AFLR4 : Min Bounding Box Length = 40
AFLR4 : Max Ref Bounding Box Length = 40
AFLR4 : Min Ref Bounding Box Length = 40
AFLR4 : Reference Length = 1.61374
AFLR4 : BL Thickness = 0
AFLR4 : Abs Min Surf Spacing = 0.00403436
AFLR4 : Min Surf Spacing = 0.161374
AFLR4 : Max Surf Spacing = 1.21031
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 w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
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 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Nodes, Trias,Quads= 1293 2452 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Nodes, Trias,Quads= 1298 2462 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 3418 6687 0
AFLR4 : Nodes, Trias,Quads= 3008 5867 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1315 2496 0
AFLR4 : Nodes, Trias,Quads= 1297 2460 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Nodes, Trias,Quads= 1298 2462 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1319 2504 0
AFLR4 : Nodes, Trias,Quads= 1294 2454 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 200 344 0
AFLR4 : Nodes, Trias,Quads= 160 264 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 193 330 0
AFLR4 : Nodes, Trias,Quads= 155 254 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 17 21 0
AFLR4 : Nodes, Trias,Quads= 11 9 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 9344 18684 928
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 9344 18684
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1335 2536 0
AFLR4 : Nodes, Trias,Quads= 1317 2500 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1337 2540 0
AFLR4 : Nodes, Trias,Quads= 1320 2506 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 3787 7420 0
AFLR4 : Nodes, Trias,Quads= 2943 5732 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1341 2548 0
AFLR4 : Nodes, Trias,Quads= 1321 2508 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 1337 2540 0
AFLR4 : Nodes, Trias,Quads= 1320 2506 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1342 2550 0
AFLR4 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 233 404 0
AFLR4 : Nodes, Trias,Quads= 210 358 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 224 386 0
AFLR4 : Nodes, Trias,Quads= 196 330 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 9478 18952 946
OVERALL : CPU Time = 0.393 seconds
Body 1 (of 1)
Number of nodes = 9478
Number of elements = 18952
Number of triangle elements = 18952
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9478
Total number of elements = 18952
Total number of triangle elements = 18952
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 61021
Number of elements = 351564
Number of triangles = 18952
Number of quadrilatarals = 0
Number of tetrahedrals = 332612
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 - Skin
Boundary condition name - SymmPlane
Done getting CFD boundary conditions
Info: No recognized data transfer names found.
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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: 0.294118.
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_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_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: 3.
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_aeroelasticSimple_Pressure_SA.dat.
Surface file name: surface_flow_aeroelasticSimple_Pressure_SA.
Volume file name: flow_aeroelasticSimple_Pressure_SA.
Restart file name: restart_flow_aeroelasticSimple_Pressure_SA.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- 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 ) -------------------
Three dimensional problem.
61021 grid points.
332612 volume elements.
3 surface markers.
12522 boundary elements in index 0 (Marker = BC_1).
5732 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
332612 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 83.4538. Mean K: 0.863308. Standard deviation K: 5.00657.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 52.4071| 86.6424|
| CV Face Area Aspect Ratio| 1.04128| 21.5651|
| CV Sub-Volume Ratio| 1| 10.4254|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 61021| 1/1.00| 10|
| 1| 10400| 1/5.87| 8.31654|
| 2| 1824| 1/5.7| 6.98282|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 9.2451 m^2.
Area projection in the x-plane = 0.651846 m^2, y-plane = 0.30478 m^2, z-plane = 4.4157 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.38 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.86329e-18 m, z-direction = -0.0467611 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
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| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
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| 1.4267e+00| -1.358658| 0.921673| 0.583457| 4.110448| -0.914331|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.4183e+00| -1.761379| 0.764232| 0.408273| 3.694369| -0.434651|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.4081e+00| -1.765424| 0.580434| 0.226849| 3.691843| 1.933305|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.76542| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticSimple_Pressure_SA.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
|CSV file |surface_flow_aeroelasticSimple_Pressure_SA.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
|Tecplot binary |flow_aeroelasticSimple_Pressure_SA.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
|Tecplot binary surface |surface_flow_aeroelasticSimple_Pressure_SA.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.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) ------------------------
Running PostAnalysis ...... su2
Running ...... astros
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Skin, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Skin, index = 1
Name = Rib_Root, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 180
Number of elements = 194
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 32
Elemental Quad4 = 162
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Rib_Root
Property name - Skin
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - pressureAero
No "groupName" specified for Load tuple pressureAero, going to use load name
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
Number of variables = 16
Number of data points = 361
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 3.100050e+09, tgt = 3.100049e+09, diff = 1.864962e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
Number of variables = 16
Number of data points = 361
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 3.018381e+09, tgt = 3.018381e+09, diff = 2.015136e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
Number of variables = 16
Number of data points = 361
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 4.368630e+07, tgt = 4.368630e+07, diff = 3.295440e-01
Extracting external pressure loads from data transfer....
TransferName = Skin_Top
Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
TransferName = Skin_Bottom
Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
TransferName = Skin_Tip
Number of Elements = 16 (total = 178)
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
real 1m35.360s
user 0m15.847s
sys 0m2.152s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Pressure_SU2_and_Astros.py passed (as expected)
=================================================
=================================================
+ echo 'aeroelasticSimple_Displacement_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Displacement_SU2_and_Astros.py test;
+ python -u aeroelasticSimple_Displacement_SU2_and_Astros.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Running PreAnalysis ...... astros
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Skin, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Skin, index = 1
Name = Rib_Root, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 180
Number of elements = 194
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 32
Elemental Quad4 = 162
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Rib_Root
Property name - Skin
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - pressureInternal
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Running PostAnalysis ...... astros
Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 1 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 9 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 12 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 0 1 2 3 4 5
EGADS : 2 Yes 0 0 1 0 1 1 3 5 6
EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8
EGADS : 4 Yes 0 0 1 0 1 1 3 5 6
EGADS : 5 Yes 0 0 1 0 1 1 2 4 6
EGADS : 6 Yes 0 0 1 0 1 2 3 4 5
EGADS : 7 Yes 0 0 1 0 1 3 8 9
EGADS : 8 Yes 0 0 1 0 1 3 7 9
EGADS : 9 Yes 0 0 1 0 1 7 8
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 5 6 -7 -1
EGADS : 3 -2 7 9 -8 -10 -11
EGADS : 4 -12 3 8 -13
EGADS : 5 4 12 -14 -5
EGADS : 6 -6 14 13 -9
EGADS : 7 15 10 -17 -16
EGADS : 8 17 11 -15 -18
EGADS : 9 16 18
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3 4
EGADS : 4 5
EGADS : 5 6
EGADS : 6 7
EGADS : 7 8
EGADS : 8 9
EGADS : 9 10
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes 1 2 -3 -4
EGADS : 2 Yes 5 6 -7 -1
EGADS : 3 Yes -2 7 9 -8
EGADS : 4 Yes -10 -11
EGADS : 5 Yes -12 3 8 -13
EGADS : 6 Yes 4 12 -14 -5
EGADS : 7 Yes -6 14 13 -9
EGADS : 8 Yes 15 10 -17 -16
EGADS : 9 Yes 17 11 -15 -18
EGADS : 10 Yes 16 18
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 2 1 1 1 2
EGADS : 2 0 Yes 1 3 1 1 3
EGADS : 3 0 Yes 4 3 1 1 4
EGADS : 4 0 Yes 2 4 1 1 5
EGADS : 5 0 Yes 2 5 1 2 5
EGADS : 6 0 Yes 5 6 1 2 6
EGADS : 7 0 Yes 1 6 1 2 3
EGADS : 8 0 Yes 3 7 1 3 4
EGADS : 9 0 Yes 6 7 1 3 6
EGADS : 10 0 Yes 8 9 1 3 7
EGADS : 11 0 Yes 9 8 1 3 8
EGADS : 12 0 Yes 4 10 1 4 5
EGADS : 13 0 Yes 10 7 1 4 6
EGADS : 14 0 Yes 5 10 1 5 6
EGADS : 15 0 Yes 11 8 1 7 8
EGADS : 16 0 Yes 11 12 1 7 9
EGADS : 17 0 Yes 12 9 1 7 8
EGADS : 18 0 Yes 12 11 1 8 9
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 0
EGADS : 2 Yes 0 40 0
EGADS : 3 Yes 0 0 20
EGADS : 4 Yes 0 40 20
EGADS : 5 Yes 20 40 0
EGADS : 6 Yes 20 0 0
EGADS : 7 Yes 20 0 20
EGADS : 8 Yes 1.61374306 0 0
EGADS : 9 Yes 0 0 0
EGADS : 10 Yes 20 40 20
EGADS : 11 Yes 2.53650745 3.87298335 0.334116517
EGADS : 12 Yes 1.57194608 3.87298335 0.249728332
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 40
AFLR4 : Min Bounding Box Length = 40
AFLR4 : Max Ref Bounding Box Length = 40
AFLR4 : Min Ref Bounding Box Length = 40
AFLR4 : Reference Length = 1.61374
AFLR4 : BL Thickness = 0
AFLR4 : Abs Min Surf Spacing = 0.00403436
AFLR4 : Min Surf Spacing = 0.161374
AFLR4 : Max Surf Spacing = 1.21031
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 w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
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 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Nodes, Trias,Quads= 1293 2452 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Nodes, Trias,Quads= 1298 2462 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 3418 6687 0
AFLR4 : Nodes, Trias,Quads= 3008 5867 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1315 2496 0
AFLR4 : Nodes, Trias,Quads= 1297 2460 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Nodes, Trias,Quads= 1298 2462 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1319 2504 0
AFLR4 : Nodes, Trias,Quads= 1294 2454 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 200 344 0
AFLR4 : Nodes, Trias,Quads= 160 264 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 193 330 0
AFLR4 : Nodes, Trias,Quads= 155 254 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 17 21 0
AFLR4 : Nodes, Trias,Quads= 11 9 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 9344 18684 928
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 9344 18684
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1335 2536 0
AFLR4 : Nodes, Trias,Quads= 1317 2500 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1337 2540 0
AFLR4 : Nodes, Trias,Quads= 1320 2506 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 3787 7420 0
AFLR4 : Nodes, Trias,Quads= 2943 5732 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1341 2548 0
AFLR4 : Nodes, Trias,Quads= 1321 2508 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 1337 2540 0
AFLR4 : Nodes, Trias,Quads= 1320 2506 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1342 2550 0
AFLR4 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 233 404 0
AFLR4 : Nodes, Trias,Quads= 210 358 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 224 386 0
AFLR4 : Nodes, Trias,Quads= 196 330 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 9478 18952 946
OVERALL : CPU Time = 0.302 seconds
Body 1 (of 1)
Number of nodes = 9478
Number of elements = 18952
Number of triangle elements = 18952
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9478
Total number of elements = 18952
Total number of triangle elements = 18952
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 61021
Number of elements = 351564
Number of triangles = 18952
Number of quadrilatarals = 0
Number of tetrahedrals = 332612
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 - Skin
Boundary condition name - SymmPlane
Done getting CFD boundary conditions
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Displacement_SA_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, 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/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
61021 grid points.
332612 volume elements.
3 surface markers.
12522 boundary elements in index 0 (Marker = BC_1).
5732 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
332612 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 63999.5.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 27.885377 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |../aflr3/aflr3_CAPS.su2 |
|CSV file |surface_deformed.csv |
|Tecplot binary |volume_deformed.szplt |
|Tecplot binary surface |surface_deformed.szplt |
Adding any FFD information to the SU2 file.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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: 0.294118.
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_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_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: 3.
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_aeroelasticSimple_Displacement_SA.dat.
Surface file name: surface_flow_aeroelasticSimple_Displacement_SA.
Volume file name: flow_aeroelasticSimple_Displacement_SA.
Restart file name: restart_flow_aeroelasticSimple_Displacement_SA.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- 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 ) -------------------
Three dimensional problem.
61021 grid points.
332612 volume elements.
3 surface markers.
12522 boundary elements in index 0 (Marker = BC_1).
5732 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
332612 tetrahedra.
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 1 TETRAHEDRON volume elements.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63997.8.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 83.9101. Mean K: 0.903406. Standard deviation K: 4.47641.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 46.1587| 86.6056|
| CV Face Area Aspect Ratio| 1.04375| 23.1726|
| CV Sub-Volume Ratio| 1| 124.296|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 61021| 1/1.00| 10|
| 1| 10400| 1/5.87| 8.31654|
| 2| 1824| 1/5.7| 6.98282|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.89892 m.
Wetted area = 11.6151 m^2.
Area projection in the x-plane = 2.90002 m^2, y-plane = 1.28883 m^2, z-plane = 4.27937 m^2.
Max. coordinate in the x-direction = 2.53729 m, y-direction = 3.89892 m, z-direction = 0.526515 m.
Min. coordinate in the x-direction = 0.000170858 m, y-direction = -2.86329e-18 m, z-direction = -0.706552 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
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| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
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| 1.8239e+00| -0.688947| 1.740396| 1.255245| 4.780159| 0.054072|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.8057e+00| -1.147407| 1.463053| 1.107626| 4.324911| 0.052353|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.8351e+00| -1.161658| 1.244069| 0.911458| 4.304744| 0.132783|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.16166| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticSimple_Displacement_SA.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat).
|CSV file |surface_flow_aeroelasticSimple_Displacement_SA.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat).
|Tecplot binary |flow_aeroelasticSimple_Displacement_SA.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat).
|Tecplot binary surface |surface_flow_aeroelasticSimple_Displacement_SA.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.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) ------------------------
Running PostAnalysis ...... su2
real 1m19.358s
user 0m52.219s
sys 0m4.554s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Displacement_SU2_and_Astros.py passed (as expected)
=================================================
=================================================
+ echo 'aeroelasticSimple_Iterative_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Iterative_SU2_and_Astros.py test;
+ python -u aeroelasticSimple_Iterative_SU2_and_Astros.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 1 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 9 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 12 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 0 1 2 3 4 5
EGADS : 2 Yes 0 0 1 0 1 1 3 5 6
EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8
EGADS : 4 Yes 0 0 1 0 1 1 3 5 6
EGADS : 5 Yes 0 0 1 0 1 1 2 4 6
EGADS : 6 Yes 0 0 1 0 1 2 3 4 5
EGADS : 7 Yes 0 0 1 0 1 3 8 9
EGADS : 8 Yes 0 0 1 0 1 3 7 9
EGADS : 9 Yes 0 0 1 0 1 7 8
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 5 6 -7 -1
EGADS : 3 -2 7 9 -8 -10 -11
EGADS : 4 -12 3 8 -13
EGADS : 5 4 12 -14 -5
EGADS : 6 -6 14 13 -9
EGADS : 7 15 10 -17 -16
EGADS : 8 17 11 -15 -18
EGADS : 9 16 18
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3 4
EGADS : 4 5
EGADS : 5 6
EGADS : 6 7
EGADS : 7 8
EGADS : 8 9
EGADS : 9 10
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes 1 2 -3 -4
EGADS : 2 Yes 5 6 -7 -1
EGADS : 3 Yes -2 7 9 -8
EGADS : 4 Yes -10 -11
EGADS : 5 Yes -12 3 8 -13
EGADS : 6 Yes 4 12 -14 -5
EGADS : 7 Yes -6 14 13 -9
EGADS : 8 Yes 15 10 -17 -16
EGADS : 9 Yes 17 11 -15 -18
EGADS : 10 Yes 16 18
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 2 1 1 1 2
EGADS : 2 0 Yes 1 3 1 1 3
EGADS : 3 0 Yes 4 3 1 1 4
EGADS : 4 0 Yes 2 4 1 1 5
EGADS : 5 0 Yes 2 5 1 2 5
EGADS : 6 0 Yes 5 6 1 2 6
EGADS : 7 0 Yes 1 6 1 2 3
EGADS : 8 0 Yes 3 7 1 3 4
EGADS : 9 0 Yes 6 7 1 3 6
EGADS : 10 0 Yes 8 9 1 3 7
EGADS : 11 0 Yes 9 8 1 3 8
EGADS : 12 0 Yes 4 10 1 4 5
EGADS : 13 0 Yes 10 7 1 4 6
EGADS : 14 0 Yes 5 10 1 5 6
EGADS : 15 0 Yes 11 8 1 7 8
EGADS : 16 0 Yes 11 12 1 7 9
EGADS : 17 0 Yes 12 9 1 7 8
EGADS : 18 0 Yes 12 11 1 8 9
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 0
EGADS : 2 Yes 0 40 0
EGADS : 3 Yes 0 0 20
EGADS : 4 Yes 0 40 20
EGADS : 5 Yes 20 40 0
EGADS : 6 Yes 20 0 0
EGADS : 7 Yes 20 0 20
EGADS : 8 Yes 1.61374306 0 0
EGADS : 9 Yes 0 0 0
EGADS : 10 Yes 20 40 20
EGADS : 11 Yes 2.53650745 3.87298335 0.334116517
EGADS : 12 Yes 1.57194608 3.87298335 0.249728332
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 40
AFLR4 : Min Bounding Box Length = 40
AFLR4 : Max Ref Bounding Box Length = 40
AFLR4 : Min Ref Bounding Box Length = 40
AFLR4 : Reference Length = 1.61374
AFLR4 : BL Thickness = 0
AFLR4 : Abs Min Surf Spacing = 0.00403436
AFLR4 : Min Surf Spacing = 0.161374
AFLR4 : Max Surf Spacing = 1.21031
AFLR4 : Global Scale Factor = 2
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 w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
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 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 376 682 0
AFLR4 : Nodes, Trias,Quads= 381 692 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 374 678 0
AFLR4 : Nodes, Trias,Quads= 380 690 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 927 1777 0
AFLR4 : Nodes, Trias,Quads= 821 1565 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 376 682 0
AFLR4 : Nodes, Trias,Quads= 380 690 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 374 678 0
AFLR4 : Nodes, Trias,Quads= 380 690 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 376 682 0
AFLR4 : Nodes, Trias,Quads= 378 686 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 63 96 0
AFLR4 : Nodes, Trias,Quads= 55 80 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 64 96 0
AFLR4 : Nodes, Trias,Quads= 57 82 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 11 13 0
AFLR4 : Nodes, Trias,Quads= 7 5 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 2592 5180 482
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 2592 5180
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 385 700 0
AFLR4 : Nodes, Trias,Quads= 380 690 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 383 696 0
AFLR4 : Nodes, Trias,Quads= 381 692 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 1004 1929 0
AFLR4 : Nodes, Trias,Quads= 955 1831 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 381 692 0
AFLR4 : Nodes, Trias,Quads= 378 686 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 386 702 0
AFLR4 : Nodes, Trias,Quads= 379 688 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 382 694 0
AFLR4 : Nodes, Trias,Quads= 379 688 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 74 115 0
AFLR4 : Nodes, Trias,Quads= 65 97 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 75 116 0
AFLR4 : Nodes, Trias,Quads= 63 92 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 2737 5470 490
OVERALL : CPU Time = 0.150 seconds
Body 1 (of 1)
Number of nodes = 2737
Number of elements = 5470
Number of triangle elements = 5470
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 2737
Total number of elements = 5470
Total number of triangle elements = 5470
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 11256
Number of elements = 63738
Number of triangles = 5470
Number of quadrilatarals = 0
Number of tetrahedrals = 58268
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 - Skin
Boundary condition name - SymmPlane
Done getting CFD boundary conditions
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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: 0.294118.
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_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_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: 3.
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_aeroelasticSimple_Iterative.dat.
Surface file name: surface_flow_aeroelasticSimple_Iterative.
Volume file name: flow_aeroelasticSimple_Iterative.
Restart file name: restart_flow_aeroelasticSimple_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- 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 ) -------------------
Three dimensional problem.
11256 grid points.
58268 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58268 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 47.1143. Mean K: 0.755831. Standard deviation K: 3.51256.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 54.7348| 84.8841|
| CV Face Area Aspect Ratio| 1.12479| 21.5536|
| CV Sub-Volume Ratio| 1| 12.6921|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11256| 1/1.00| 10|
| 1| 1996| 1/5.64| 8.4272|
| 2| 403| 1/4.95| 7.41577|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 8.08979 m^2.
Area projection in the x-plane = 0.572014 m^2, y-plane = 0.261888 m^2, z-plane = 3.84035 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.380358 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.8602e-18 m, z-direction = -0.0467106 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
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| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
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| 3.5050e-01| -0.789536| 1.510409| 1.185966| 4.679570| -1.041016|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.6164e-01| -1.127407| 1.420277| 1.033530| 4.327735| -0.786336|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.6421e-01| -1.175401| 1.283946| 0.880440| 4.278343| -0.132156|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.1754| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|CSV file |surface_flow_aeroelasticSimple_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary |flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.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) ------------------------
Running PostAnalysis ...... su2
Running PreAnalysis ...... su2
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Skin, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Skin, index = 1
Name = Rib_Root, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 180
Number of elements = 194
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 32
Elemental Quad4 = 162
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Rib_Root
Property name - Skin
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - pressureAero
No "groupName" specified for Load tuple pressureAero, going to use load name
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 3.096760e+09, tgt = 3.096760e+09, diff = 1.492910e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 3.011695e+09, tgt = 3.011694e+09, diff = 1.923570e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 4.109026e+07, tgt = 4.109026e+07, diff = 4.061875e-02
Extracting external pressure loads from data transfer....
TransferName = Skin_Top
Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
TransferName = Skin_Bottom
Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
TransferName = Skin_Tip
Number of Elements = 16 (total = 178)
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, 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/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
11256 grid points.
58268 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58268 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 63999.5.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 1.310705 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |../aflr3/aflr3_CAPS.su2 |
|CSV file |surface_deformed.csv |
|Tecplot binary |volume_deformed.szplt |
|Tecplot binary surface |surface_deformed.szplt |
Adding any FFD information to the SU2 file.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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: 0.294118.
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_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_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: 3.
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_aeroelasticSimple_Iterative.dat.
Surface file name: surface_flow_aeroelasticSimple_Iterative.
Volume file name: flow_aeroelasticSimple_Iterative.
Restart file name: restart_flow_aeroelasticSimple_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- 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 ) -------------------
Three dimensional problem.
11256 grid points.
58268 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58268 tetrahedra.
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 833 TETRAHEDRON volume elements.
There has been a re-orientation of 48 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 64447.4.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 22.7937. Mean K: 0.531652. Standard deviation K: 1.7548.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 3.7227| 84.4835|
| CV Face Area Aspect Ratio| 1.10495| 238.499|
| CV Sub-Volume Ratio| 1| 13912.3|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11256| 1/1.00| 10|
| 1| 1998| 1/5.63| 8.43002|
| 2| 402| 1/4.97| 7.40963|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 4.55968 m.
Wetted area = 160.827 m^2.
Area projection in the x-plane = 64.3603 m^2, y-plane = 35.1581 m^2, z-plane = 5.47205 m^2.
Max. coordinate in the x-direction = 2.76437 m, y-direction = 4.55968 m, z-direction = 13.7319 m.
Min. coordinate in the x-direction = -0.725355 m, y-direction = -0.052136 m, z-direction = -19.2849 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
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| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
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| 4.0735e-01| 1.824113| 4.775982| 4.842363| 7.293219| 0.008847|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 4.1244e-01| 2.168766| 4.752124| 4.914849| 7.681778| -0.045048|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 4.1417e-01| 2.398967| 4.879748| 5.073235| 7.882468| -0.102393|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 2.39897| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|CSV file |surface_flow_aeroelasticSimple_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary |flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 36 non-physical points in the solution.
--------------------------- 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) ------------------------
Running PostAnalysis ...... su2
Running PreAnalysis ...... su2
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 1.917724e+09, tgt = 1.917724e+09, diff = 1.324418e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 1.656893e+09, tgt = 1.656892e+09, diff = 6.779244e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 2.957264e+07, tgt = 2.957264e+07, diff = 1.998837e-02
Extracting external pressure loads from data transfer....
TransferName = Skin_Top
Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
TransferName = Skin_Bottom
Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
TransferName = Skin_Tip
Number of Elements = 16 (total = 178)
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, 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/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
11256 grid points.
58268 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58268 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 833 TETRAHEDRON volume elements.
There has been a re-orientation of 48 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 64447.4.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 9.478450 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |../aflr3/aflr3_CAPS.su2 |
|CSV file |surface_deformed.csv |
|Tecplot binary |volume_deformed.szplt |
|Tecplot binary surface |surface_deformed.szplt |
Adding any FFD information to the SU2 file.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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: 0.294118.
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_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_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: 3.
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_aeroelasticSimple_Iterative.dat.
Surface file name: surface_flow_aeroelasticSimple_Iterative.
Volume file name: flow_aeroelasticSimple_Iterative.
Restart file name: restart_flow_aeroelasticSimple_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- 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 ) -------------------
Three dimensional problem.
11256 grid points.
58268 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58268 tetrahedra.
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 14399 TETRAHEDRON volume elements.
There has been a re-orientation of 524 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 70569.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 256.759. Mean K: 2.42121. Standard deviation K: 11.8787.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 1.4983| 82.5649|
| CV Face Area Aspect Ratio| 1.08119| 668.774|
| CV Sub-Volume Ratio| 1| 341229|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11256| 1/1.00| 10|
| 1| 1988| 1/5.66| 8.41593|
| 2| 406| 1/4.9| 7.43412|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.1784 m.
Wetted area = 179.433 m^2.
Area projection in the x-plane = 88.7848 m^2, y-plane = 36.3704 m^2, z-plane = 3.46068 m^2.
Max. coordinate in the x-direction = 1.67522 m, y-direction = 3.1784 m, z-direction = 57.9541 m.
Min. coordinate in the x-direction = -1.65404 m, y-direction = -0.0174089 m, z-direction = -7.07709 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
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| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
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| 3.9791e-01| 2.432844| 5.401867| 5.352270| 7.901950| 6.472864|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 4.0033e-01| 2.821000| 5.419905| 5.356527| 8.237468| -0.076947|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 4.0660e-01| 2.904903| 5.494465| 5.350945| 8.293229| -0.060150|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 2.9049| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|CSV file |surface_flow_aeroelasticSimple_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary |flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 176 non-physical points in the solution.
Warning: 42 reconstructed states for upwinding are non-physical.
--------------------------- 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) ------------------------
Running PostAnalysis ...... su2
Running PreAnalysis ...... su2
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 1.259137e+09, tgt = 1.259137e+09, diff = 2.759926e+01
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 1.085342e+09, tgt = 1.085342e+09, diff = 2.598397e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 8.759534e+06, tgt = 8.759534e+06, diff = 3.619500e-03
Extracting external pressure loads from data transfer....
TransferName = Skin_Top
Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
TransferName = Skin_Bottom
Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
TransferName = Skin_Tip
Number of Elements = 16 (total = 178)
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, 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/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
11256 grid points.
58268 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58268 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 14399 TETRAHEDRON volume elements.
There has been a re-orientation of 524 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 70569.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 37.497450 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |../aflr3/aflr3_CAPS.su2 |
|CSV file |surface_deformed.csv |
|Tecplot binary |volume_deformed.szplt |
|Tecplot binary surface |surface_deformed.szplt |
Adding any FFD information to the SU2 file.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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: 0.294118.
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_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_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: 3.
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_aeroelasticSimple_Iterative.dat.
Surface file name: surface_flow_aeroelasticSimple_Iterative.
Volume file name: flow_aeroelasticSimple_Iterative.
Restart file name: restart_flow_aeroelasticSimple_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- 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 ) -------------------
Three dimensional problem.
11256 grid points.
58268 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58268 tetrahedra.
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 15363 TETRAHEDRON volume elements.
There has been a re-orientation of 1625 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 5.20959e+08.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 87.4916. Mean K: 0.94402. Standard deviation K: 3.51469.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 1.81072| 82.6934|
| CV Face Area Aspect Ratio| 1.07582| 1695.62|
| CV Sub-Volume Ratio| 1| 4.03202e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11256| 1/1.00| 10|
| 1| 1999| 1/5.63| 8.43142|
| 2| 401| 1/4.99| 7.40348|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 1.70423 m.
Wetted area = 3176.01 m^2.
Area projection in the x-plane = 846.94 m^2, y-plane = 1086.32 m^2, z-plane = 93.2217 m^2.
Max. coordinate in the x-direction = 8.55784 m, y-direction = 1.70423 m, z-direction = 382.765 m.
Min. coordinate in the x-direction = 0.0351752 m, y-direction = -26.4792 m, z-direction = -0.0657664 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
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| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
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| 3.2222e-01| 5.498448| 8.465297| 8.420082| 10.967553| -0.047127|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.3013e-01| 6.085734| 8.634641| 8.516137| 11.372290| -0.046479|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.2019e-01| 6.142769| 8.794761| 8.545661| 11.519221| -0.046486|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 6.14277| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|CSV file |surface_flow_aeroelasticSimple_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary |flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 464 non-physical points in the solution.
Warning: 54 reconstructed states for upwinding are non-physical.
--------------------------- 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) ------------------------
Running PostAnalysis ...... su2
Cl = -246.780871
Cd = 5308.69692
real 1m29.849s
user 1m5.177s
sys 0m4.548s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Iterative_SU2_and_Astros.py passed (as expected)
=================================================
=================================================
+ echo 'aeroelastic_Iterative_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
aeroelastic_Iterative_SU2_and_Astros.py test;
+ python -u aeroelastic_Iterative_SU2_and_Astros.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 1 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 9 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 12 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 0 1 2 3 4 5
EGADS : 2 Yes 0 0 1 0 1 1 3 5 6
EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8
EGADS : 4 Yes 0 0 1 0 1 1 3 5 6
EGADS : 5 Yes 0 0 1 0 1 1 2 4 6
EGADS : 6 Yes 0 0 1 0 1 2 3 4 5
EGADS : 7 Yes 0 0 1 0 1 3 8 9
EGADS : 8 Yes 0 0 1 0 1 3 7 9
EGADS : 9 Yes 0 0 1 0 1 7 8
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 5 6 -7 -1
EGADS : 3 -2 7 9 -8 -10 -11
EGADS : 4 -12 3 8 -13
EGADS : 5 4 12 -14 -5
EGADS : 6 -6 14 13 -9
EGADS : 7 15 10 -17 -16
EGADS : 8 17 11 -15 -18
EGADS : 9 16 18
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3 4
EGADS : 4 5
EGADS : 5 6
EGADS : 6 7
EGADS : 7 8
EGADS : 8 9
EGADS : 9 10
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes 1 2 -3 -4
EGADS : 2 Yes 5 6 -7 -1
EGADS : 3 Yes -2 7 9 -8
EGADS : 4 Yes -10 -11
EGADS : 5 Yes -12 3 8 -13
EGADS : 6 Yes 4 12 -14 -5
EGADS : 7 Yes -6 14 13 -9
EGADS : 8 Yes 15 10 -17 -16
EGADS : 9 Yes 17 11 -15 -18
EGADS : 10 Yes 16 18
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 2 1 1 1 2
EGADS : 2 0 Yes 1 3 1 1 3
EGADS : 3 0 Yes 4 3 1 1 4
EGADS : 4 0 Yes 2 4 1 1 5
EGADS : 5 0 Yes 2 5 1 2 5
EGADS : 6 0 Yes 5 6 1 2 6
EGADS : 7 0 Yes 1 6 1 2 3
EGADS : 8 0 Yes 3 7 1 3 4
EGADS : 9 0 Yes 6 7 1 3 6
EGADS : 10 0 Yes 8 9 1 3 7
EGADS : 11 0 Yes 9 8 1 3 8
EGADS : 12 0 Yes 4 10 1 4 5
EGADS : 13 0 Yes 10 7 1 4 6
EGADS : 14 0 Yes 5 10 1 5 6
EGADS : 15 0 Yes 11 8 1 7 8
EGADS : 16 0 Yes 11 12 1 7 9
EGADS : 17 0 Yes 12 9 1 7 8
EGADS : 18 0 Yes 12 11 1 8 9
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 0
EGADS : 2 Yes 0 40 0
EGADS : 3 Yes 0 0 20
EGADS : 4 Yes 0 40 20
EGADS : 5 Yes 20 40 0
EGADS : 6 Yes 20 0 0
EGADS : 7 Yes 20 0 20
EGADS : 8 Yes 1.61374306 0 0
EGADS : 9 Yes 0 0 0
EGADS : 10 Yes 20 40 20
EGADS : 11 Yes 2.53650745 3.87298335 0.334116517
EGADS : 12 Yes 1.57194608 3.87298335 0.249728332
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 40
AFLR4 : Min Bounding Box Length = 40
AFLR4 : Max Ref Bounding Box Length = 40
AFLR4 : Min Ref Bounding Box Length = 40
AFLR4 : Reference Length = 1.61374
AFLR4 : BL Thickness = 0
AFLR4 : Abs Min Surf Spacing = 0.00403436
AFLR4 : Min Surf Spacing = 0.161374
AFLR4 : Max Surf Spacing = 1.21031
AFLR4 : Global Scale Factor = 2
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 w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
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 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 376 682 0
AFLR4 : Nodes, Trias,Quads= 381 692 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 374 678 0
AFLR4 : Nodes, Trias,Quads= 380 690 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 927 1777 0
AFLR4 : Nodes, Trias,Quads= 821 1565 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 376 682 0
AFLR4 : Nodes, Trias,Quads= 380 690 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 374 678 0
AFLR4 : Nodes, Trias,Quads= 380 690 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 376 682 0
AFLR4 : Nodes, Trias,Quads= 378 686 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 63 96 0
AFLR4 : Nodes, Trias,Quads= 55 80 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 64 96 0
AFLR4 : Nodes, Trias,Quads= 57 82 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 11 13 0
AFLR4 : Nodes, Trias,Quads= 7 5 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 2592 5180 482
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 2592 5180
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 385 700 0
AFLR4 : Nodes, Trias,Quads= 380 690 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 383 696 0
AFLR4 : Nodes, Trias,Quads= 381 692 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 1004 1929 0
AFLR4 : Nodes, Trias,Quads= 955 1831 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 381 692 0
AFLR4 : Nodes, Trias,Quads= 378 686 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 386 702 0
AFLR4 : Nodes, Trias,Quads= 379 688 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 382 694 0
AFLR4 : Nodes, Trias,Quads= 379 688 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 74 115 0
AFLR4 : Nodes, Trias,Quads= 65 97 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 75 116 0
AFLR4 : Nodes, Trias,Quads= 63 92 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 2737 5470 490
OVERALL : CPU Time = 0.147 seconds
Body 1 (of 1)
Number of nodes = 2737
Number of elements = 5470
Number of triangle elements = 5470
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 2737
Total number of elements = 5470
Total number of triangle elements = 5470
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 11256
Number of elements = 63738
Number of triangles = 5470
Number of quadrilatarals = 0
Number of tetrahedrals = 58268
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 - Skin
Boundary condition name - SymmPlane
Done getting CFD boundary conditions
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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: 0.294118.
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_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_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: 3.
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_aeroelastic_Iterative.dat.
Surface file name: surface_flow_aeroelastic_Iterative.
Volume file name: flow_aeroelastic_Iterative.
Restart file name: restart_flow_aeroelastic_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- 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 ) -------------------
Three dimensional problem.
11256 grid points.
58268 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58268 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 47.1143. Mean K: 0.755831. Standard deviation K: 3.51256.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 54.7348| 84.8841|
| CV Face Area Aspect Ratio| 1.12479| 21.5536|
| CV Sub-Volume Ratio| 1| 12.6921|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11256| 1/1.00| 10|
| 1| 1996| 1/5.64| 8.4272|
| 2| 403| 1/4.95| 7.41577|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 8.08979 m^2.
Area projection in the x-plane = 0.572014 m^2, y-plane = 0.261888 m^2, z-plane = 3.84035 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.380358 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.8602e-18 m, z-direction = -0.0467106 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
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| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
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| 3.6969e-01| -0.789536| 1.510409| 1.185966| 4.679570| -1.041016|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.8284e-01| -1.127407| 1.420277| 1.033530| 4.327735| -0.786336|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.8498e-01| -1.175401| 1.283946| 0.880440| 4.278343| -0.132156|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.1754| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelastic_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|CSV file |surface_flow_aeroelastic_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary |flow_aeroelastic_Iterative.szplt |
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.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) ------------------------
Running PostAnalysis ...... su2
Running PreAnalysis ...... su2
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Ribs_and_Spars, index = 1
Name = Skin, index = 2
Name = Rib_Root, index = 3
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 746
Number of elements = 898
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 120
Elemental Quad4 = 778
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - Rib_Root
Property name - Ribs_and_Spars
Property name - Skin
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - pressureAero
No "groupName" specified for Load tuple pressureAero, going to use load name
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 3.096760e+09, tgt = 3.096760e+09, diff = 7.750620e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 3.011695e+09, tgt = 3.011695e+09, diff = 5.915480e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 4.109026e+07, tgt = 4.109027e+07, diff = 9.559192e+00
Extracting external pressure loads from data transfer....
TransferName = Skin_Top
Number of Elements = 330 (total = 330)
Extracting external pressure loads from data transfer....
TransferName = Skin_Bottom
Number of Elements = 330 (total = 660)
Extracting external pressure loads from data transfer....
TransferName = Skin_Tip
Number of Elements = 30 (total = 690)
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, 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/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
11256 grid points.
58268 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58268 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 63999.5.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 1.949143 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |../aflr3/aflr3_CAPS.su2 |
|CSV file |surface_deformed.csv |
|Tecplot binary |volume_deformed.szplt |
|Tecplot binary surface |surface_deformed.szplt |
Adding any FFD information to the SU2 file.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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: 0.294118.
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_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_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: 3.
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_aeroelastic_Iterative.dat.
Surface file name: surface_flow_aeroelastic_Iterative.
Volume file name: flow_aeroelastic_Iterative.
Restart file name: restart_flow_aeroelastic_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- 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 ) -------------------
Three dimensional problem.
11256 grid points.
58268 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58268 tetrahedra.
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 16754 TETRAHEDRON volume elements.
There has been a re-orientation of 938 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 142536.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 322.181. Mean K: 2.74718. Standard deviation K: 15.019.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 3.27553| 84.0444|
| CV Face Area Aspect Ratio| 1.0902| 8197.63|
| CV Sub-Volume Ratio| 1| 130596|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11256| 1/1.00| 10|
| 1| 1972| 1/5.71| 8.39329|
| 2| 403| 1/4.89| 7.41577|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 14.8698 m.
Wetted area = 1600.51 m^2.
Area projection in the x-plane = 475.22 m^2, y-plane = 496.48 m^2, z-plane = 68.0269 m^2.
Max. coordinate in the x-direction = 3.82443 m, y-direction = 14.8698 m, z-direction = 28.3133 m.
Min. coordinate in the x-direction = -13.8591 m, y-direction = -0.831658 m, z-direction = -110.549 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
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| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
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| 4.1428e-01| 2.948801| 5.913937| 6.360939| 8.417907| 0.522837|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 4.2216e-01| 3.536742| 6.046544| 6.328864| 9.032488| 0.275751|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 4.1670e-01| 3.558693| 5.991304| 6.317634| 9.016026| 0.318018|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 3.55869| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelastic_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|CSV file |surface_flow_aeroelastic_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary |flow_aeroelastic_Iterative.szplt |
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 88 non-physical points in the solution.
Warning: 1 reconstructed states for upwinding are non-physical.
--------------------------- 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) ------------------------
Running PostAnalysis ...... su2
Running PreAnalysis ...... su2
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 1.106105e+09, tgt = 1.106105e+09, diff = 3.421523e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 1.354175e+09, tgt = 1.354175e+09, diff = 3.991435e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 5.937583e+06, tgt = 5.937591e+06, diff = 8.092772e+00
Extracting external pressure loads from data transfer....
TransferName = Skin_Top
Number of Elements = 330 (total = 330)
Extracting external pressure loads from data transfer....
TransferName = Skin_Bottom
Number of Elements = 330 (total = 660)
Extracting external pressure loads from data transfer....
TransferName = Skin_Tip
Number of Elements = 30 (total = 690)
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, 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/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
11256 grid points.
58268 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58268 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 16754 TETRAHEDRON volume elements.
There has been a re-orientation of 938 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 142536.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 37.002042 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |../aflr3/aflr3_CAPS.su2 |
|CSV file |surface_deformed.csv |
|Tecplot binary |volume_deformed.szplt |
|Tecplot binary surface |surface_deformed.szplt |
Adding any FFD information to the SU2 file.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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: 0.294118.
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_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_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: 3.
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_aeroelastic_Iterative.dat.
Surface file name: surface_flow_aeroelastic_Iterative.
Volume file name: flow_aeroelastic_Iterative.
Restart file name: restart_flow_aeroelastic_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- 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 ) -------------------
Three dimensional problem.
11256 grid points.
58268 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58268 tetrahedra.
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 31421 TETRAHEDRON volume elements.
There has been a re-orientation of 1523 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 7.74252e+07.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 147.166. Mean K: 1.11112. Standard deviation K: 4.47278.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 0.0168051| 81.3317|
| CV Face Area Aspect Ratio| 1.51547| 1329.08|
| CV Sub-Volume Ratio| 1| 471327|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11256| 1/1.00| 10|
| 1| 2004| 1/5.62| 8.43845|
| 2| 407| 1/4.92| 7.44022|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 8.54195 m.
Wetted area = 34429.3 m^2.
Area projection in the x-plane = 26169.7 m^2, y-plane = 733.092 m^2, z-plane = 265.001 m^2.
Max. coordinate in the x-direction = 4.32665 m, y-direction = 8.54195 m, z-direction = 874.585 m.
Min. coordinate in the x-direction = -10.8982 m, y-direction = -56.5428 m, z-direction = -84.5772 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
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| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
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| 3.8391e-01| 4.978313| 7.941628| 8.059022| 10.447419| 0.005737|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 4.0266e-01| 5.351219| 7.914017| 7.922766| 10.745141| 0.005628|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 4.0534e-01| 5.393166| 7.903703| 7.948539| 10.745858| 0.005964|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 5.39317| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelastic_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|CSV file |surface_flow_aeroelastic_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary |flow_aeroelastic_Iterative.szplt |
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 731 non-physical points in the solution.
Warning: 42 reconstructed states for upwinding are non-physical.
--------------------------- 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) ------------------------
Running PostAnalysis ...... su2
Running PreAnalysis ...... su2
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 1.368284e+09, tgt = 1.368283e+09, diff = 5.762926e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 1.260984e+09, tgt = 1.260984e+09, diff = 2.208813e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 1.625040e+07, tgt = 1.625049e+07, diff = 9.465821e+01
Extracting external pressure loads from data transfer....
TransferName = Skin_Top
Number of Elements = 330 (total = 330)
Extracting external pressure loads from data transfer....
TransferName = Skin_Bottom
Number of Elements = 330 (total = 660)
Extracting external pressure loads from data transfer....
TransferName = Skin_Tip
Number of Elements = 30 (total = 690)
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, 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/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
11256 grid points.
58268 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58268 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 31421 TETRAHEDRON volume elements.
There has been a re-orientation of 1523 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 7.74252e+07.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 38.000816 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |../aflr3/aflr3_CAPS.su2 |
|CSV file |surface_deformed.csv |
|Tecplot binary |volume_deformed.szplt |
|Tecplot binary surface |surface_deformed.szplt |
Adding any FFD information to the SU2 file.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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: 0.294118.
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_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_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: 3.
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_aeroelastic_Iterative.dat.
Surface file name: surface_flow_aeroelastic_Iterative.
Volume file name: flow_aeroelastic_Iterative.
Restart file name: restart_flow_aeroelastic_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- 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 ) -------------------
Three dimensional problem.
11256 grid points.
58268 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58268 tetrahedra.
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 37377 TETRAHEDRON volume elements.
There has been a re-orientation of 1850 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.8337e+12.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 15.3324. Mean K: 0.315098. Standard deviation K: 0.939574.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 0.715655| 82.734|
| CV Face Area Aspect Ratio| 1.55074| 181547|
| CV Sub-Volume Ratio| 1| 4.52475e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11256| 1/1.00| 10|
| 1| 1985| 1/5.67| 8.41169|
| 2| 414| 1/4.79| 7.48264|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 162.871 m.
Wetted area = 140455 m^2.
Area projection in the x-plane = 51232.7 m^2, y-plane = 31274.8 m^2, z-plane = 1708.01 m^2.
Max. coordinate in the x-direction = 22.9192 m, y-direction = 162.871 m, z-direction = 10.0607 m.
Min. coordinate in the x-direction = -7.41198 m, y-direction = -2.71044 m, z-direction = -2210.71 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
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| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
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| 4.0226e-01| 7.937102| 10.903956| 10.831517| 13.406208| -0.022639|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 4.1560e-01| 8.457601| 11.035115| 10.891929| 13.856119| -0.024471|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 4.1906e-01| 8.536485| 11.055638| 10.976332| 13.858301| -0.027539|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 8.53649| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelastic_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|CSV file |surface_flow_aeroelastic_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary |flow_aeroelastic_Iterative.szplt |
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 532 non-physical points in the solution.
Warning: 103 reconstructed states for upwinding are non-physical.
--------------------------- 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) ------------------------
Running PostAnalysis ...... su2
real 2m25.472s
user 2m14.593s
sys 0m10.862s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aeroelastic_Iterative_SU2_and_Astros.py passed (as expected)
=================================================
=================================================
+ echo 'aeroelasticSimple_Temperature_SU2_and_TACS.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Temperature_SU2_and_TACS.py test;
+ python -u aeroelasticSimple_Temperature_SU2_and_TACS.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 1 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 9 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 12 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 0 1 2 3 4 5
EGADS : 2 Yes 0 0 1 0 1 1 3 5 6
EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8
EGADS : 4 Yes 0 0 1 0 1 1 3 5 6
EGADS : 5 Yes 0 0 1 0 1 1 2 4 6
EGADS : 6 Yes 0 0 1 0 1 2 3 4 5
EGADS : 7 Yes 0 0 1 0 1 3 8 9
EGADS : 8 Yes 0 0 1 0 1 3 7 9
EGADS : 9 Yes 0 0 1 0 1 7 8
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 5 6 -7 -1
EGADS : 3 -2 7 9 -8 -10 -11
EGADS : 4 -12 3 8 -13
EGADS : 5 4 12 -14 -5
EGADS : 6 -6 14 13 -9
EGADS : 7 15 10 -17 -16
EGADS : 8 17 11 -15 -18
EGADS : 9 16 18
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3 4
EGADS : 4 5
EGADS : 5 6
EGADS : 6 7
EGADS : 7 8
EGADS : 8 9
EGADS : 9 10
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes 1 2 -3 -4
EGADS : 2 Yes 5 6 -7 -1
EGADS : 3 Yes -2 7 9 -8
EGADS : 4 Yes -10 -11
EGADS : 5 Yes -12 3 8 -13
EGADS : 6 Yes 4 12 -14 -5
EGADS : 7 Yes -6 14 13 -9
EGADS : 8 Yes 15 10 -17 -16
EGADS : 9 Yes 17 11 -15 -18
EGADS : 10 Yes 16 18
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 2 1 1 1 2
EGADS : 2 0 Yes 1 3 1 1 3
EGADS : 3 0 Yes 4 3 1 1 4
EGADS : 4 0 Yes 2 4 1 1 5
EGADS : 5 0 Yes 2 5 1 2 5
EGADS : 6 0 Yes 5 6 1 2 6
EGADS : 7 0 Yes 1 6 1 2 3
EGADS : 8 0 Yes 3 7 1 3 4
EGADS : 9 0 Yes 6 7 1 3 6
EGADS : 10 0 Yes 8 9 1 3 7
EGADS : 11 0 Yes 9 8 1 3 8
EGADS : 12 0 Yes 4 10 1 4 5
EGADS : 13 0 Yes 10 7 1 4 6
EGADS : 14 0 Yes 5 10 1 5 6
EGADS : 15 0 Yes 11 8 1 7 8
EGADS : 16 0 Yes 11 12 1 7 9
EGADS : 17 0 Yes 12 9 1 7 8
EGADS : 18 0 Yes 12 11 1 8 9
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 0
EGADS : 2 Yes 0 40 0
EGADS : 3 Yes 0 0 20
EGADS : 4 Yes 0 40 20
EGADS : 5 Yes 20 40 0
EGADS : 6 Yes 20 0 0
EGADS : 7 Yes 20 0 20
EGADS : 8 Yes 1.61374306 0 0
EGADS : 9 Yes 0 0 0
EGADS : 10 Yes 20 40 20
EGADS : 11 Yes 2.53650745 3.87298335 0.334116517
EGADS : 12 Yes 1.57194608 3.87298335 0.249728332
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 40
AFLR4 : Min Bounding Box Length = 40
AFLR4 : Max Ref Bounding Box Length = 40
AFLR4 : Min Ref Bounding Box Length = 40
AFLR4 : Reference Length = 1.61374
AFLR4 : BL Thickness = 0
AFLR4 : Abs Min Surf Spacing = 0.00403436
AFLR4 : Min Surf Spacing = 0.161374
AFLR4 : Max Surf Spacing = 1.21031
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 w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
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 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Nodes, Trias,Quads= 1293 2452 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Nodes, Trias,Quads= 1298 2462 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 3418 6687 0
AFLR4 : Nodes, Trias,Quads= 3008 5867 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1315 2496 0
AFLR4 : Nodes, Trias,Quads= 1297 2460 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Nodes, Trias,Quads= 1298 2462 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1319 2504 0
AFLR4 : Nodes, Trias,Quads= 1294 2454 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 200 344 0
AFLR4 : Nodes, Trias,Quads= 160 264 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 193 330 0
AFLR4 : Nodes, Trias,Quads= 155 254 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 17 21 0
AFLR4 : Nodes, Trias,Quads= 11 9 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 9344 18684 928
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 9344 18684
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1335 2536 0
AFLR4 : Nodes, Trias,Quads= 1317 2500 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1337 2540 0
AFLR4 : Nodes, Trias,Quads= 1320 2506 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 3787 7420 0
AFLR4 : Nodes, Trias,Quads= 2943 5732 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1341 2548 0
AFLR4 : Nodes, Trias,Quads= 1321 2508 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 1337 2540 0
AFLR4 : Nodes, Trias,Quads= 1320 2506 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1342 2550 0
AFLR4 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 233 404 0
AFLR4 : Nodes, Trias,Quads= 210 358 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 224 386 0
AFLR4 : Nodes, Trias,Quads= 196 330 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 9478 18952 946
OVERALL : CPU Time = 0.351 seconds
Body 1 (of 1)
Number of nodes = 9478
Number of elements = 18952
Number of triangle elements = 18952
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9478
Total number of elements = 18952
Total number of triangle elements = 18952
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 61021
Number of elements = 351564
Number of triangles = 18952
Number of quadrilatarals = 0
Number of tetrahedrals = 332612
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 - Skin
Boundary condition name - SymmPlane
Done getting CFD boundary conditions
Info: No recognized data transfer names found.
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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: 0.294118.
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_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_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: 3.
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_aeroelasticSimple_Temperature_SM.dat.
Surface file name: surface_flow_aeroelasticSimple_Temperature_SM.
Volume file name: flow_aeroelasticSimple_Temperature_SM.
Restart file name: restart_flow_aeroelasticSimple_Temperature_SM.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- 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 ) -------------------
Three dimensional problem.
61021 grid points.
332612 volume elements.
3 surface markers.
12522 boundary elements in index 0 (Marker = BC_1).
5732 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
332612 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 83.4538. Mean K: 0.863308. Standard deviation K: 5.00657.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 52.4071| 86.6424|
| CV Face Area Aspect Ratio| 1.04128| 21.5651|
| CV Sub-Volume Ratio| 1| 10.4254|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 61021| 1/1.00| 10|
| 1| 10400| 1/5.87| 8.31654|
| 2| 1824| 1/5.7| 6.98282|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 9.2451 m^2.
Area projection in the x-plane = 0.651846 m^2, y-plane = 0.30478 m^2, z-plane = 4.4157 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.38 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.86329e-18 m, z-direction = -0.0467611 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
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| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
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| 1.8846e+00| -1.358658| 0.921673| 0.583457| 4.110448| -0.914331|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.8058e+00| -1.761379| 0.764232| 0.408273| 3.694369| -0.434651|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.8646e+00| -1.765424| 0.580434| 0.226849| 3.691843| 1.933305|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.76542| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticSimple_Temperature_SM.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat).
|CSV file |surface_flow_aeroelasticSimple_Temperature_SM.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat).
|Tecplot binary |flow_aeroelasticSimple_Temperature_SM.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat).
|Tecplot binary surface |surface_flow_aeroelasticSimple_Temperature_SM.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.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) ------------------------
Running PostAnalysis ...... su2
Running PreAnalysis ...... tacs
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Skin, index = 1
Name = Rib_Root, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 12
Number of elements = 12
Number of triangle elements = 4
Number of quadrilateral elements = 8
----------------------------
Total number of nodes = 12
Total number of elements = 12
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Skin, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Skin, index = 1
Name = Rib_Root, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 12
Number of elements = 12
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4
Elemental Quad4 = 8
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Rib_Root
Property name - Skin
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - Skin
No "groupName" specified for Load tuple Skin, going to use load name
Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Skin, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Skin, index = 1
Name = Rib_Root, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 12
Number of elements = 12
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4
Elemental Quad4 = 8
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv
Number of variables = 16
Number of data points = 361
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Temperature'
Rank 0: src = 1.497162e+03, tgt = 1.497162e+03, diff = 3.256482e-07
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Skin, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Skin, index = 1
Name = Rib_Root, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 12
Number of elements = 12
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4
Elemental Quad4 = 8
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv
Number of variables = 16
Number of data points = 361
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Temperature'
Rank 0: src = 1.453298e+03, tgt = 1.453298e+03, diff = 2.530585e-07
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Skin, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Skin, index = 1
Name = Rib_Root, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 12
Number of elements = 12
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4
Elemental Quad4 = 8
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv
Number of variables = 16
Number of data points = 361
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Temperature'
Rank 0: src = 2.097780e+01, tgt = 2.097780e+01, diff = 3.733902e-12
Extracting external thermal loads from data transfer....
TransferName = Skin_Top
Number of Nodes = 9 (total = 9)
Extracting external thermal loads from data transfer....
TransferName = Skin_Bottom
Number of Nodes = 9 (total = 18)
Extracting external thermal loads from data transfer....
TransferName = Skin_Tip
Number of Nodes = 4 (total = 16)
Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Running PostAnalysis ...... tacs
real 0m24.999s
user 0m20.089s
sys 0m2.238s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Temperature_SU2_and_TACS.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Did not run examples for:
Mystran
=================================================
All tests pass!
=================================================
=================================================
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/legacy/examples/regressionTest
++ ./execute_PyTestRegression.sh AEROELASTIC
=================================================
Legacy Using python : /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/ESP/venv/bin/python
=================================================
Running.... AEROELASTIC PyTests
=================================================
+ rm -rf aeroelasticSimple_Pressure_SU2_and_Astros
+ echo 'aeroelasticSimple_Pressure_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Pressure_SU2_and_Astros.py test;
+ python -u aeroelasticSimple_Pressure_SU2_and_Astros.py -verbosity=0 -workDir=runDirectory -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Running PreAnalysis ...... tetgen
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Running PostAnalysis ...... tetgen
Body 1 (of 1)
Number of nodes = 12449
Number of elements = 24894
Number of triangle elements = 24894
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 12449
Total number of elements = 24894
Running PreAnalysis ...... tetgen
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Number of surface: nodes - 12449, elements - 24894
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Running PostAnalysis ...... tetgen
Running PreAnalysis ...... su2
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Skin
Boundary condition name - SymmPlane
Done getting CFD boundary conditions
Info: No recognized data transfer names found.
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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: 0.294118.
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_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../runDirectory_AeroelasticSimple_Pressure_tetgen_tetgenAIM/tetgen_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: 5.
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_aeroelasticSimple_Pressure_SA.dat.
Surface file name: surface_flow_aeroelasticSimple_Pressure_SA.
Volume file name: flow_aeroelasticSimple_Pressure_SA.
Restart file name: restart_flow_aeroelasticSimple_Pressure_SA.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- 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 ) -------------------
Three dimensional problem.
22559 grid points.
98644 volume elements.
3 surface markers.
342 boundary elements in index 0 (Marker = BC_1).
12856 boundary elements in index 1 (Marker = BC_2).
11696 boundary elements in index 2 (Marker = BC_3).
98644 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 1594.52. Mean K: 49.8216. Standard deviation K: 81.7526.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 12.7569| 83.9993|
| CV Face Area Aspect Ratio| 1.80581| 23185.6|
| CV Sub-Volume Ratio| 1| 77755.6|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 22559| 1/1.00| 10|
| 1| 4207| 1/5.36| 8.56989|
| 2| 987| 1/4.26| 7.92833|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 10.0438 m^2.
Area projection in the x-plane = 0.679139 m^2, y-plane = 0.327414 m^2, z-plane = 4.84583 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.380458 m.
Min. coordinate in the x-direction = -0.000478065 m, y-direction = -2.86151e-18 m, z-direction = -0.0467319 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
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| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
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| 6.8784e-01| -1.523015| 0.609935| 0.080731| 3.946091| -0.730159|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 6.6957e-01| -1.304187| 1.158339| 0.940576| 4.166256| -0.217956|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 6.6438e-01| -1.429691| 1.178606| 1.010958| 4.033394| 2.094727|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 6.3526e-01| -1.367153| 1.041900| 0.919423| 4.096463| -17.368218|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 5.9986e-01| -1.451051| 0.942431| 0.855378| 4.011094| -8.664140|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.45105| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticSimple_Pressure_SA.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
|CSV file |surface_flow_aeroelasticSimple_Pressure_SA.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
|Tecplot binary |flow_aeroelasticSimple_Pressure_SA.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
|Tecplot binary surface |surface_flow_aeroelasticSimple_Pressure_SA.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.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) ------------------------
Running PostAnalysis ...... su2
Executing dataTransfer ......
No variable name provided - defaulting to variable - Pressure
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Skin, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Skin, index = 1
Name = Rib_Root, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 180
Number of elements = 194
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 32
Elemental Quad4 = 162
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Rib_Root
Property name - Skin
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - pressureAero
No "groupName" specified for Load tuple pressureAero, going to use load name
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
Number of variables = 16
Number of data points = 5887
No variable name provided - defaulting to variable - Pressure
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
Number of variables = 16
Number of data points = 5887
No variable name provided - defaulting to variable - Pressure
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
Number of variables = 16
Number of data points = 5887
Running PreAnalysis ...... astros
Extracting external pressure loads from data transfer....
TransferName = Skin_Top
Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
TransferName = Skin_Bottom
Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
TransferName = Skin_Tip
Number of Elements = 16 (total = 178)
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Running PostAnalysis ...... astros
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.aimName' is deprecated. Please use 'name'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsAnalysis.getAnalysisInfo' is deprecated. Please use 'Analysis.info'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsBound.fillVertexSets' is deprecated. Please use 'None'!
WARNING: 'capsAnalysis.getAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsBound.executeTransfer' is deprecated. Please use 'None'!
WARNING: 'capsBound.getDestData' is deprecated. Please use 'vertexSet["name"].dataSet["variableName"].getData'!
WARNING: 'DataSet.getData' is deprecated. Please use 'DataSet.data'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m28.845s
user 0m15.067s
sys 0m1.930s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case aeroelasticSimple_Pressure_SU2_and_Astros.py passed (as expected)
=================================================
=================================================
+ rm -rf aeroelasticSimple_Displacement_SU2_and_Astros
+ echo 'aeroelasticSimple_Displacement_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Displacement_SU2_and_Astros.py test;
+ python -u aeroelasticSimple_Displacement_SU2_and_Astros.py -verbosity=0 -workDir=runDirectory -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Running PreAnalysis ...... tetgen
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Running PostAnalysis ...... tetgen
Body 1 (of 1)
Number of nodes = 12449
Number of elements = 24894
Number of triangle elements = 24894
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 12449
Total number of elements = 24894
Running PreAnalysis ...... tetgen
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Number of surface: nodes - 12449, elements - 24894
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Running PostAnalysis ...... tetgen
Running PreAnalysis ...... astros
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Skin, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Skin, index = 1
Name = Rib_Root, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 180
Number of elements = 194
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 32
Elemental Quad4 = 162
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Rib_Root
Property name - Skin
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - pressureInternal
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Running PostAnalysis ...... astros
Executing dataTransfer ......
No variable name provided - defaulting to variable - Displacement
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Skin
Boundary condition name - SymmPlane
Done getting CFD boundary conditions
No variable name provided - defaulting to variable - Displacement
No variable name provided - defaulting to variable - Displacement
Running PreAnalysis ...... su2
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Displacement_SA_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, 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/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../runDirectory_AeroelasticSimple_Displacement_tetgen_tetgenAIM/tetgen_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../runDirectory_AeroelasticSimple_Displacement_tetgen_tetgenAIM/tetgen_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
22559 grid points.
98644 volume elements.
3 surface markers.
342 boundary elements in index 0 (Marker = BC_1).
12856 boundary elements in index 1 (Marker = BC_2).
11696 boundary elements in index 2 (Marker = BC_3).
98644 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 63999.5.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 2.238274 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |../runDirectory_AeroelasticSimple_Displacement_tetgen_tetgenAIM/tetgen_CAPS.su2|
|CSV file |surface_deformed.csv |
|Tecplot binary |volume_deformed.szplt |
|Tecplot binary surface |surface_deformed.szplt |
Adding any FFD information to the SU2 file.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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: 0.294118.
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_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../runDirectory_AeroelasticSimple_Displacement_tetgen_tetgenAIM/tetgen_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: 5.
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_aeroelasticSimple_Displacement_SA.dat.
Surface file name: surface_flow_aeroelasticSimple_Displacement_SA.
Volume file name: flow_aeroelasticSimple_Displacement_SA.
Restart file name: restart_flow_aeroelasticSimple_Displacement_SA.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- 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 ) -------------------
Three dimensional problem.
22559 grid points.
98644 volume elements.
3 surface markers.
342 boundary elements in index 0 (Marker = BC_1).
12856 boundary elements in index 1 (Marker = BC_2).
11696 boundary elements in index 2 (Marker = BC_3).
98644 tetrahedra.
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 4164 TETRAHEDRON volume elements.
There has been a re-orientation of 721 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63997.7.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 1963.01. Mean K: 62.1337. Standard deviation K: 144.97.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 4.10523| 83.0894|
| CV Face Area Aspect Ratio| 1.79967| 21772.3|
| CV Sub-Volume Ratio| 1.00009| 1.15114e+07|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 22559| 1/1.00| 10|
| 1| 4216| 1/5.35| 8.576|
| 2| 994| 1/4.24| 7.94703|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.89957 m.
Wetted area = 12.4772 m^2.
Area projection in the x-plane = 3.08369 m^2, y-plane = 1.33891 m^2, z-plane = 4.78464 m^2.
Max. coordinate in the x-direction = 2.53729 m, y-direction = 3.89957 m, z-direction = 0.526515 m.
Min. coordinate in the x-direction = -0.00039489 m, y-direction = -2.86151e-18 m, z-direction = -0.706932 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
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| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
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| 5.4274e-01| -0.781959| 1.689594| 1.305458| 4.687147| 0.026467|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 5.4981e-01| -0.460038| 2.013474| 1.780488| 5.017361| -0.000510|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 5.6972e-01| -0.646472| 2.043898| 1.872141| 4.822937| 0.009300|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 5.5902e-01| -0.706944| 1.989522| 1.799633| 4.759822| 0.025851|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 5.6155e-01| -0.672257| 1.916984| 1.673304| 4.795683| 0.046289|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -0.672257| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticSimple_Displacement_SA.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat).
|CSV file |surface_flow_aeroelasticSimple_Displacement_SA.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat).
|Tecplot binary |flow_aeroelasticSimple_Displacement_SA.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat).
|Tecplot binary surface |surface_flow_aeroelasticSimple_Displacement_SA.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat).
+-----------------------------------------------------------------------+
Warning: there are 356 non-physical points in the solution.
Warning: 149 reconstructed states for upwinding are non-physical.
--------------------------- 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) ------------------------
Running PostAnalysis ...... su2
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.aimName' is deprecated. Please use 'name'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsAnalysis.getAnalysisInfo' is deprecated. Please use 'Analysis.info'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsBound.fillVertexSets' is deprecated. Please use 'None'!
WARNING: 'capsBound.executeTransfer' is deprecated. Please use 'None'!
WARNING: 'capsBound.getDestData' is deprecated. Please use 'vertexSet["name"].dataSet["variableName"].getData'!
WARNING: 'DataSet.getData' is deprecated. Please use 'DataSet.data'!
WARNING: 'capsAnalysis.getAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m24.132s
user 0m19.390s
sys 0m2.846s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case aeroelasticSimple_Displacement_SU2_and_Astros.py passed (as expected)
=================================================
=================================================
+ rm -rf aeroelasticSimple_Iterative_SU2_and_Astros
+ echo 'aeroelasticSimple_Iterative_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Iterative_SU2_and_Astros.py test;
+ python -u aeroelasticSimple_Iterative_SU2_and_Astros.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Running PreAnalysis ...... egads
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Running PostAnalysis ...... egads
Body 1 (of 1)
Number of nodes = 12449
Number of elements = 24894
Number of triangle elements = 24894
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 12449
Total number of elements = 24894
Running PreAnalysis ...... tetgen
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Number of surface: nodes - 12449, elements - 24894
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.898385
Creating surface mesh ...
Surface mesh seconds: 0.029414
Recovering boundaries...
Boundary recovery seconds: 0.10842
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.028991
Recovering Delaunayness...
Delaunay recovery seconds: 0.02886
Refining mesh...
16594 insertions, added 9193 points, 319384 tetrahedra in queue.
5525 insertions, added 626 points, 65154 tetrahedra in queue.
7365 insertions, added 240 points, 1338 tetrahedra in queue.
Refinement seconds: 1.43175
Smoothing vertices...
Mesh smoothing seconds: 0.851848
Improving mesh...
Mesh improvement seconds: 0.023173
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.007267
Total running seconds: 3.40852
Statistics:
Input points: 12449
Input facets: 24894
Input segments: 37341
Input holes: 0
Input regions: 0
Mesh points: 22559
Mesh tetrahedra: 98644
Mesh faces: 209735
Mesh faces on exterior boundary: 24894
Mesh faces on input facets: 24894
Mesh edges on input segments: 37341
Steiner points inside domain: 10110
Done meshing using TetGen!
Running PostAnalysis ...... tetgen
Executing dataTransfer "Displacement"......
Running PreAnalysis ...... su2
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Skin
Boundary condition name - SymmPlane
Done getting CFD boundary conditions
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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: 0.294118.
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_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../runDirectory_AeroelasticSimple_Iterative_SA_tetgen_tetgenAIM/tetgen_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: 5.
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_aeroelasticSimple_Iterative.dat.
Surface file name: surface_flow_aeroelasticSimple_Iterative.
Volume file name: flow_aeroelasticSimple_Iterative.
Restart file name: restart_flow_aeroelasticSimple_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- 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 ) -------------------
Three dimensional problem.
22559 grid points.
98644 volume elements.
3 surface markers.
342 boundary elements in index 0 (Marker = BC_1).
12856 boundary elements in index 1 (Marker = BC_2).
11696 boundary elements in index 2 (Marker = BC_3).
98644 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 1594.52. Mean K: 49.8216. Standard deviation K: 81.7526.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 12.7569| 83.9993|
| CV Face Area Aspect Ratio| 1.80581| 23185.6|
| CV Sub-Volume Ratio| 1| 77755.6|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 22559| 1/1.00| 10|
| 1| 4207| 1/5.36| 8.56989|
| 2| 987| 1/4.26| 7.92833|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 10.0438 m^2.
Area projection in the x-plane = 0.679139 m^2, y-plane = 0.327414 m^2, z-plane = 4.84583 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.380458 m.
Min. coordinate in the x-direction = -0.000478065 m, y-direction = -2.86151e-18 m, z-direction = -0.0467319 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
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| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
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| 4.4337e-01| -1.523015| 0.609935| 0.080731| 3.946091| -0.730159|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 4.4007e-01| -1.304187| 1.158339| 0.940576| 4.166256| -0.217956|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 4.4234e-01| -1.429691| 1.178606| 1.010958| 4.033394| 2.094727|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 4.4752e-01| -1.367153| 1.041900| 0.919423| 4.096463| -17.368218|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 4.4337e-01| -1.451051| 0.942431| 0.855378| 4.011094| -8.664140|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.45105| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|CSV file |surface_flow_aeroelasticSimple_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary |flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.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) ------------------------
Running PostAnalysis ...... su2
Executing dataTransfer "Pressure"......
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Skin, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Skin, index = 1
Name = Rib_Root, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 180
Number of elements = 194
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 32
Elemental Quad4 = 162
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Rib_Root
Property name - Skin
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - pressureAero
No "groupName" specified for Load tuple pressureAero, going to use load name
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 5887
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 5887
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 5887
Running PreAnalysis ...... astros
Extracting external pressure loads from data transfer....
TransferName = Skin_Top
Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
TransferName = Skin_Bottom
Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
TransferName = Skin_Tip
Number of Elements = 16 (total = 178)
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Running PostAnalysis ...... astros
Executing dataTransfer "Displacement"......
Running PreAnalysis ...... su2
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, 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/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../runDirectory_AeroelasticSimple_Iterative_SA_tetgen_tetgenAIM/tetgen_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../runDirectory_AeroelasticSimple_Iterative_SA_tetgen_tetgenAIM/tetgen_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
22559 grid points.
98644 volume elements.
3 surface markers.
342 boundary elements in index 0 (Marker = BC_1).
12856 boundary elements in index 1 (Marker = BC_2).
11696 boundary elements in index 2 (Marker = BC_3).
98644 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 63999.5.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 2.013268 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |../runDirectory_AeroelasticSimple_Iterative_SA_tetgen_tetgenAIM/tetgen_CAPS.su2|
|CSV file |surface_deformed.csv |
|Tecplot binary |volume_deformed.szplt |
|Tecplot binary surface |surface_deformed.szplt |
Adding any FFD information to the SU2 file.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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: 0.294118.
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_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../runDirectory_AeroelasticSimple_Iterative_SA_tetgen_tetgenAIM/tetgen_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: 5.
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_aeroelasticSimple_Iterative.dat.
Surface file name: surface_flow_aeroelasticSimple_Iterative.
Volume file name: flow_aeroelasticSimple_Iterative.
Restart file name: restart_flow_aeroelasticSimple_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- 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 ) -------------------
Three dimensional problem.
22559 grid points.
98644 volume elements.
3 surface markers.
342 boundary elements in index 0 (Marker = BC_1).
12856 boundary elements in index 1 (Marker = BC_2).
11696 boundary elements in index 2 (Marker = BC_3).
98644 tetrahedra.
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 21981 TETRAHEDRON volume elements.
There has been a re-orientation of 3560 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 70780.7.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 3476.02. Mean K: 44.3899. Standard deviation K: 174.259.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 0.294588| 82.35|
| CV Face Area Aspect Ratio| 1.59729| 264565|
| CV Sub-Volume Ratio| 1.00237| 9.68698e+08|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 22559| 1/1.00| 10|
| 1| 4216| 1/5.35| 8.576|
| 2| 1006| 1/4.19| 7.97888|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 8.64457 m.
Wetted area = 422.06 m^2.
Area projection in the x-plane = 127.222 m^2, y-plane = 150.625 m^2, z-plane = 17.3669 m^2.
Max. coordinate in the x-direction = 3.25205 m, y-direction = 8.64457 m, z-direction = 5.77239 m.
Min. coordinate in the x-direction = -0.150417 m, y-direction = -2.86151e-18 m, z-direction = -69.8353 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
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| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
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| 5.3039e-01| 2.497833| 5.464549| 5.493406| 7.966939| -0.147599|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 5.3284e-01| 2.635820| 5.357309| 5.420465| 8.064943| -0.212663|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 5.3122e-01| 2.745159| 5.333528| 5.403812| 8.165941| -0.256643|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 5.2497e-01| 2.848543| 5.362919| 5.427791| 8.162681| -0.188291|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 5.1969e-01| 2.898930| 5.471261| 5.476218| 8.244534| -0.162863|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 2.89893| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|CSV file |surface_flow_aeroelasticSimple_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary |flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 1125 non-physical points in the solution.
Warning: 513 reconstructed states for upwinding are non-physical.
--------------------------- 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) ------------------------
Running PostAnalysis ...... su2
Executing dataTransfer "Pressure"......
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 5887
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 5887
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 5887
Running PreAnalysis ...... astros
Extracting external pressure loads from data transfer....
TransferName = Skin_Top
Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
TransferName = Skin_Bottom
Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
TransferName = Skin_Tip
Number of Elements = 16 (total = 178)
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Running PostAnalysis ...... astros
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: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsAnalysis.getAnalysisInfo' is deprecated. Please use 'Analysis.info'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsBound.fillVertexSets' is deprecated. Please use 'None'!
WARNING: 'capsBound.executeTransfer' is deprecated. Please use 'None'!
WARNING: 'capsBound.getDestData' is deprecated. Please use 'vertexSet["name"].dataSet["variableName"].getData'!
WARNING: 'DataSet.getData' is deprecated. Please use 'DataSet.data'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 1m13.358s
user 0m21.090s
sys 0m2.954s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case aeroelasticSimple_Iterative_SU2_and_Astros.py passed (as expected)
=================================================
=================================================
+ rm -rf aeroelastic_Iterative_SU2_and_Astros
+ echo 'aeroelastic_Iterative_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
aeroelastic_Iterative_SU2_and_Astros.py test;
+ python -u aeroelastic_Iterative_SU2_and_Astros.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Running PreAnalysis ...... egads
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Running PostAnalysis ...... egads
Body 1 (of 1)
Number of nodes = 25819
Number of elements = 51634
Number of triangle elements = 51634
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 25819
Total number of elements = 51634
Running PreAnalysis ...... tetgen
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Number of surface: nodes - 25819, elements - 51634
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 2.41114
Creating surface mesh ...
Surface mesh seconds: 0.085025
Recovering boundaries...
Boundary recovery seconds: 0.293466
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.093961
Recovering Delaunayness...
Delaunay recovery seconds: 0.06451
Refining mesh...
34416 insertions, added 14656 points, 515068 tetrahedra in queue.
11460 insertions, added 501 points, 93186 tetrahedra in queue.
15276 insertions, added 385 points, 6920 tetrahedra in queue.
Refinement seconds: 19.1219
Smoothing vertices...
Mesh smoothing seconds: 1.94074
Improving mesh...
Mesh improvement seconds: 0.054753
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.022013
Total running seconds: 24.0884
Statistics:
Input points: 25819
Input facets: 51634
Input segments: 77451
Input holes: 0
Input regions: 0
Mesh points: 41966
Mesh tetrahedra: 173588
Mesh faces: 372993
Mesh faces on exterior boundary: 51634
Mesh faces on input facets: 51634
Mesh edges on input segments: 77451
Steiner points inside domain: 16147
Done meshing using TetGen!
Running PostAnalysis ...... tetgen
Executing dataTransfer "Displacement"......
Running PreAnalysis ...... su2
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Skin
Boundary condition name - SymmPlane
Done getting CFD boundary conditions
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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: 0.294118.
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_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../runDirectory_Aeroelastic_Iterative_SA_tetgen_tetgenAIM/tetgen_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: 5.
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_aeroelastic_Iterative.dat.
Surface file name: surface_flow_aeroelastic_Iterative.
Volume file name: flow_aeroelastic_Iterative.
Restart file name: restart_flow_aeroelastic_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- 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 ) -------------------
Three dimensional problem.
41966 grid points.
173588 volume elements.
3 surface markers.
534 boundary elements in index 0 (Marker = BC_1).
31605 boundary elements in index 1 (Marker = BC_2).
19495 boundary elements in index 2 (Marker = BC_3).
173588 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 1061.04. Mean K: 24.6984. Standard deviation K: 62.0805.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 6.17732| 85.0593|
| CV Face Area Aspect Ratio| 1.67567| 13243.7|
| CV Sub-Volume Ratio| 1| 203352|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 41966| 1/1.00| 10|
| 1| 7997| 1/5.25| 8.63179|
| 2| 1924| 1/4.16| 8.05289|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 10.1964 m^2.
Area projection in the x-plane = 0.682432 m^2, y-plane = 0.335222 m^2, z-plane = 4.92026 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.380458 m.
Min. coordinate in the x-direction = -0.000478065 m, y-direction = -2.86151e-18 m, z-direction = -0.0467319 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
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| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
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| 1.1501e+00| -1.910877| 0.181600| -0.221602| 3.558228| -0.654949|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.2138e+00| -1.276786| 1.056348| 0.859623| 4.197535| -0.247732|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.1928e+00| -1.296162| 1.234750| 1.052145| 4.173195| 1.987333|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.1507e+00| -1.109196| 1.173381| 1.032120| 4.355240| -13.040977|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.1203e+00| -0.796285| 1.368670| 0.988769| 4.677226| -7.874010|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -0.796285| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelastic_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|CSV file |surface_flow_aeroelastic_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary |flow_aeroelastic_Iterative.szplt |
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.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) ------------------------
Running PostAnalysis ...... su2
Executing dataTransfer "Pressure"......
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Ribs_and_Spars, index = 1
Name = Skin, index = 2
Name = Rib_Root, index = 3
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 746
Number of elements = 898
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 120
Elemental Quad4 = 778
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - Rib_Root
Property name - Ribs_and_Spars
Property name - Skin
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - pressureAero
No "groupName" specified for Load tuple pressureAero, going to use load name
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 9800
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 9800
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 9800
Running PreAnalysis ...... astros
Extracting external pressure loads from data transfer....
TransferName = Skin_Top
Number of Elements = 330 (total = 330)
Extracting external pressure loads from data transfer....
TransferName = Skin_Bottom
Number of Elements = 330 (total = 660)
Extracting external pressure loads from data transfer....
TransferName = Skin_Tip
Number of Elements = 30 (total = 690)
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Running PostAnalysis ...... astros
Executing dataTransfer "Displacement"......
Running PreAnalysis ...... su2
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, 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/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../runDirectory_Aeroelastic_Iterative_SA_tetgen_tetgenAIM/tetgen_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../runDirectory_Aeroelastic_Iterative_SA_tetgen_tetgenAIM/tetgen_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
41966 grid points.
173588 volume elements.
3 surface markers.
534 boundary elements in index 0 (Marker = BC_1).
31605 boundary elements in index 1 (Marker = BC_2).
19495 boundary elements in index 2 (Marker = BC_3).
173588 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 63999.5.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 4.795728 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |../runDirectory_Aeroelastic_Iterative_SA_tetgen_tetgenAIM/tetgen_CAPS.su2|
|CSV file |surface_deformed.csv |
|Tecplot binary |volume_deformed.szplt |
|Tecplot binary surface |surface_deformed.szplt |
Adding any FFD information to the SU2 file.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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: 0.294118.
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_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../runDirectory_Aeroelastic_Iterative_SA_tetgen_tetgenAIM/tetgen_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: 5.
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_aeroelastic_Iterative.dat.
Surface file name: surface_flow_aeroelastic_Iterative.
Volume file name: flow_aeroelastic_Iterative.
Restart file name: restart_flow_aeroelastic_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- 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 ) -------------------
Three dimensional problem.
41966 grid points.
173588 volume elements.
3 surface markers.
534 boundary elements in index 0 (Marker = BC_1).
31605 boundary elements in index 1 (Marker = BC_2).
19495 boundary elements in index 2 (Marker = BC_3).
173588 tetrahedra.
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 79053 TETRAHEDRON volume elements.
There has been a re-orientation of 21812 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 8.35716e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 112078. Mean K: 29.9202. Standard deviation K: 1077.84.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 0.0499425| 87.3832|
| CV Face Area Aspect Ratio| 1.74501| 4.71002e+16|
| CV Sub-Volume Ratio| 1.00083| 1.81918e+09|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 41966| 1/1.00| 10|
| 1| 8002| 1/5.24| 8.63359|
| 2| 1944| 1/4.12| 8.0807|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 53.5038 m.
Wetted area = 19247.6 m^2.
Area projection in the x-plane = 6141.41 m^2, y-plane = 6386.67 m^2, z-plane = 371.345 m^2.
Max. coordinate in the x-direction = 11.4788 m, y-direction = 53.5038 m, z-direction = 20.7885 m.
Min. coordinate in the x-direction = -2.11918 m, y-direction = -0.798855 m, z-direction = -697.391 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
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| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
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| 1.4128e+00| 4.464829| 7.431942| 7.458154| 9.933935| -0.021870|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.3827e+00| 4.631801| 7.372252| 7.315231| 10.064444| -0.016898|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.3763e+00| 4.753740| 7.478673| 7.380864| 10.292131| -0.024022|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.3736e+00| 4.917891| 7.608523| 7.447672| 10.376358| -0.020319|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.3433e+00| 4.935340| 7.615357| 7.520516| 10.436208| -0.015719|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 4.93534| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelastic_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|CSV file |surface_flow_aeroelastic_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary |flow_aeroelastic_Iterative.szplt |
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 1485 non-physical points in the solution.
Warning: 743 reconstructed states for upwinding are non-physical.
--------------------------- 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) ------------------------
Running PostAnalysis ...... su2
Executing dataTransfer "Pressure"......
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 9800
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 9800
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 9800
Running PreAnalysis ...... astros
Extracting external pressure loads from data transfer....
TransferName = Skin_Top
Number of Elements = 330 (total = 330)
Extracting external pressure loads from data transfer....
TransferName = Skin_Bottom
Number of Elements = 330 (total = 660)
Extracting external pressure loads from data transfer....
TransferName = Skin_Tip
Number of Elements = 30 (total = 690)
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Running PostAnalysis ...... astros
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: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsAnalysis.getAnalysisInfo' is deprecated. Please use 'Analysis.info'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsBound.fillVertexSets' is deprecated. Please use 'None'!
WARNING: 'capsBound.executeTransfer' is deprecated. Please use 'None'!
WARNING: 'capsBound.getDestData' is deprecated. Please use 'vertexSet["name"].dataSet["variableName"].getData'!
WARNING: 'DataSet.getData' is deprecated. Please use 'DataSet.data'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 2m6.454s
user 1m28.972s
sys 0m9.456s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case aeroelastic_Iterative_SU2_and_Astros.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Legacy Did not run examples for:
Mystran
=================================================
All tests pass!
=================================================
=================================================
[Execution node] check if [macys] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64')
[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: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64')
[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: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN64')
[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_RegCaps/CASREV=7.7,ESPTEST=CAPS/AEROELASTIC,ESP_ARCH=DARWIN64,buildnode=macys #679'.
[Checks API] No suitable checks publisher found.
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] done
Finished: SUCCESS