Started by upstream project "ESP_RegCaps" build number 665
originally caused by:
Started by an SCM change
Running as SYSTEM
[EnvInject] - Loading node environment variables.
Building remotely on reynolds in workspace /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Done
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Updating svn+ssh://acdl.mit.edu/home/svnroot/EGADS at revision '2024-06-22T22:19:10.439 -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 2050
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Updating svn+ssh://acdl.mit.edu/home/svnroot/CAPS at revision '2024-06-22T22:19:10.439 -0400'
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Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
A training/lectures
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 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
A training/lectures/session11.tex
A training/lectures/MUDDYoptions.tex
A training/lectures/muddy_01_02.tex
A training/lectures/muddy_03_04_05.tex
A training/lectures/session05.tex
A training/lectures/session06.tex
A training/lectures/session07.tex
A training/lectures/session10.tex
A training/lectures/session01.tex
A training/lectures/session03.tex
A training/lectures/welcome.tex
A training/lectures/session06
AU training/lectures/session06/inviscidWing_ScaleFactor.png
AU training/lectures/session06/inviscidTransport1.png
AU training/lectures/session06/inviscidTransport2.png
AU training/lectures/session06/inviscidTransport3.png
AU training/lectures/session06/inviscidWingPod_Prox1.png
AU training/lectures/session06/inviscidWingPod_Prox2.png
AU training/lectures/session06/inviscidWing_Body.png
AU training/lectures/session06/inviscidWing_Box.png
AU training/lectures/session06/inviscidWing_BoxFF5.png
AU training/lectures/session06/inviscidWing_LenFrac1.png
AU training/lectures/session06/inviscidWing_LenFrac2.png
AU training/lectures/session06/inviscidWing_LenFrac3.png
AU training/lectures/session06/inviscidWing_erw_all.png
AU training/lectures/session06/inviscidWing_tess.png
AU training/lectures/session06/viscousWingPod_prox2.png
AU training/lectures/session06/viscousWingPod_prox3.png
AU training/lectures/session06/viscousTransport1.png
AU training/lectures/session06/viscousTransport2.png
AU training/lectures/session06/viscousTransport3.png
AU training/lectures/session06/inviscidWing_AFLR3.png
AU training/lectures/session06/viscousWingPod_AFLR3_BL.png
AU training/lectures/session06/viscousWing_AFLR3_BL.png
AU training/lectures/session06/inviscidWingPod_Prox3.png
AU training/lectures/session06/inviscidWing_LenFrac_5.png
AU training/lectures/session06/viscousWingPod_prox1.png
AU training/lectures/session06/inviscidWing_prox.png
AU training/lectures/session06/viscousWingPod_prox.png
A training/lectures/session05
AU training/lectures/session05/avl_viewGeometry.png
AU training/lectures/session05/transport_viewGeometry.png
A training/lectures/session05/plane.avl
AU training/lectures/session05/avl_transport.png
AU training/lectures/session05/avl_transport_control.png
AU training/lectures/session05/csm_avl_transport.png
AU training/lectures/session05/csm_avl_transport_control.png
A training/lectures/session07
AU training/lectures/session07/inviscidWingPod_SourceSpace1.png
AU training/lectures/session07/inviscidWingPod_SourceSpace2.png
AU training/lectures/session07/inviscidWing_Decay1.png
AU training/lectures/session07/inviscidWing_Decay2.png
AU training/lectures/session07/inviscidWing_Decay3.png
AU training/lectures/session07/inviscidWing_Default.png
AU training/lectures/session07/inviscidWing_TRex.png
AU training/lectures/session07/inviscidWing_Turn1.png
AU training/lectures/session07/inviscidWing_Turn2.png
AU training/lectures/session07/inviscidWing_Turn3.png
AU training/lectures/session07/inviscidWing_TurnHard1.png
AU training/lectures/session07/inviscidWing_TurnHard2.png
AU training/lectures/session07/inviscidWing_TurnHard3.png
AU training/lectures/session07/AssembleTolerance.png
AU training/lectures/session07/Adapt.png
AU training/lectures/session07/SourceNearFieldBox.png
AU training/lectures/session07/SourceNearFieldMesh.png
AU training/lectures/session07/SourceSideViewMesh.png
AU training/lectures/session07/noAdapt.png
AU training/lectures/session07/inviscidTransport_Full.png
AU training/lectures/session07/inviscidTransport_Tail.png
AU training/lectures/session07/inviscidTransport_Wing.png
AU training/lectures/session07/viscousTransport_Full.png
AU training/lectures/session07/viscousTransport_Tail.png
AU training/lectures/session07/viscousTransport_Wing.png
AU training/lectures/session07/viscousWingPod_BL.png
AU training/lectures/session07/viscousWing_BL.png
A training/lectures/session09
AU training/lectures/session09/wing3_ESP_full.png
AU training/lectures/session09/wing3_ESP_ignore.png
AU training/lectures/session09/wing_TFI.png
AU training/lectures/session09/wing_dev1.png
AU training/lectures/session09/wing_dev2.png
AU training/lectures/session09/wing_dev3.png
AU training/lectures/session09/wing_dihedral1.png
AU training/lectures/session09/wing_dihedral2.png
AU training/lectures/session09/wing_dihedral3.png
AU training/lectures/session09/wing_leadingeEdge.png
AU training/lectures/session09/wing_maxLen1.png
AU training/lectures/session09/wing_maxLen2.png
AU training/lectures/session09/wing_maxLen3.png
AU training/lectures/session09/wing_mesh_size1.png
AU training/lectures/session09/wing_mesh_size2.png
AU training/lectures/session09/wing_mesh_size3.png
AU training/lectures/session09/wing_noTFI.png
AU training/lectures/session09/wing_quad1.png
AU training/lectures/session09/wing_quad2.png
AU training/lectures/session09/wing_quad3.png
AU training/lectures/session09/wing_rootLeadingEdge.png
AU training/lectures/session09/wingbox.png
AU training/lectures/session09/wingbox_mesh_size1.png
AU training/lectures/session09/wingbox_mesh_size2.png
AU training/lectures/session09/wingbox_mesh_size22.png
AU training/lectures/session09/wingbox_mesh_size3.png
AU training/lectures/session09/wingbox_mesh_size4.png
AU training/lectures/session09/wingbox_mesh_size5.png
AU training/lectures/session09/wingbox_mesh_size6.png
AU training/lectures/session09/wingbox_mesh_size7.png
AU training/lectures/session09/wingfull.png
AU training/lectures/session09/airside0.png
AU training/lectures/session09/airside1.png
AU training/lectures/session09/cyl1.png
AU training/lectures/session09/cyl2.png
AU training/lectures/session09/cyl3.png
AU training/lectures/session09/trisplit.png
AU training/lectures/session09/wing3.png
A training/lectures/session10
AU training/lectures/session10/capsLoad.png
AU training/lectures/session10/leftWingSkin.png
AU training/lectures/session10/riteWingSkin.png
AU training/lectures/session10/rootClamped.png
AU training/lectures/session10/rootSupport.png
AU training/lectures/session10/wing3_flutter_aero.png
AU training/lectures/session10/wing3_flutter_struc.png
AU training/lectures/session10/wingRib.png
AU training/lectures/session10/wingSpar1.png
AU training/lectures/session10/wingSpar2.png
AU training/lectures/session10/wing_u.png
AU training/lectures/session10/wing_v.png
AU training/lectures/session10/wing_leftCsys.png
AU training/lectures/session10/wing_riteCsys.png
A training/lectures/session11
AU training/lectures/session11/capsBound_Aero_lowerWing.png
AU training/lectures/session11/capsBound_Aero_tipWing.png
AU training/lectures/session11/capsBound_Aero_upperWing.png
AU training/lectures/session11/capsBound_Struct_lowerWing.png
AU training/lectures/session11/capsBound_Struct_tipWing.png
AU training/lectures/session11/capsBound_Struct_upperWing.png
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
AU training/lectures/session04/wing4.png
AU training/lectures/session04/wing4_CFDvisc.png
AU training/lectures/session04/wing4_VLM.png
AU training/lectures/session04/wing4_coupled.png
AU training/lectures/session04/wing4_struct.png
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
AU training/lectures/session01/inviscidTransport_Full.png
A training/lectures/session08
A training/lectures/session08/logoSU2_v3_3_mod.png
AU training/lectures/session08/hi_lift2.jpg
AU training/lectures/session08/hl_crm_01.png
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
AU training/lectures/ParaviewBasics/Screen Shot 2019-04-26 at 12.41.32 PM.png
AU training/lectures/ParaviewBasics/Screen Shot 2019-04-26 at 12.42.43 PM.png
AU training/lectures/ParaviewBasics/Screen Shot 2019-04-26 at 12.43.22 PM.png
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AU training/lectures/ParaviewBasics/Screen Shot 2019-04-26 at 12.44.04 PM.png
AU training/lectures/ParaviewBasics/Screen Shot 2019-04-26 at 12.44.13 PM.png
AU training/lectures/ParaviewBasics/Screen Shot 2019-04-26 at 12.44.53 PM.png
AU training/lectures/ParaviewBasics/Screen Shot 2019-04-26 at 12.45.27 PM.png
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AU training/lectures/ParaviewBasics/Screen Shot 2019-04-26 at 12.46.10 PM.png
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AU training/lectures/ParaviewBasics/Screen Shot 2019-04-26 at 12.46.46 PM.png
AU training/lectures/ParaviewBasics/Screen Shot 2019-05-24 at 10.44.44 AM.png
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
U doc/Makefile
At revision 4228
Cleaning up /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/JenkinsESP
Updating svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-06-22T22:19:10.439 -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’
U ESP_email.template
At revision 872
Cleaning up /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/OpenCSM/trunk/src
Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/src at revision '2024-06-22T22:19:10.439 -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’
U OpenCSM.c
At revision 2508
Cleaning up /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/OpenCSM/trunk/udc
Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/udc at revision '2024-06-22T22:19:10.439 -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 2508
Cleaning up /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/OpenCSM/trunk/data
Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/data at revision '2024-06-22T22:19:10.439 -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’
U basic/seqnum1.csm
U basic/seqnum10.csm
U basic/seqnum2.csm
U basic/seqnum3.csm
U basic/seqnum4.csm
U basic/seqnum5.csm
U basic/seqnum6.csm
U basic/seqnum7.csm
U basic/seqnum8.csm
U basic/seqnum9.csm
A Slugs
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
A Slugs/verify_7.8.0/boxHole_1.vfy
A Slugs/verify_7.8.0/box_1.vfy
A Slugs/verify_7.8.0/cylinderHole_1.vfy
A Slugs/verify_7.8.0/cylinder_1.vfy
A Slugs/verify_7.8.0/damaged_2.vfy
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
A Slugs/verify_7.8.0/pieslice_1.vfy
A Slugs/verify_7.8.0/sphere_1.vfy
A Slugs/verify_7.8.0/torus_1.vfy
A Slugs/verify_7.8.0/tutorial1.vfy
A Slugs/verify_7.8.0/wing_1.vfy
AU Slugs/damaged_1.stl
A Slugs/verify_7.7.0
A Slugs/verify_7.7.0/blend12_1.vfy
A Slugs/verify_7.7.0/blindeye_1.vfy
A Slugs/verify_7.7.0/boxBall_1.vfy
A Slugs/verify_7.7.0/boxHole_1.vfy
A Slugs/verify_7.7.0/box_1.vfy
A Slugs/verify_7.7.0/cylinderHole_1.vfy
A Slugs/verify_7.7.0/cylinder_1.vfy
A Slugs/verify_7.7.0/damaged_2.vfy
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 2508
Cleaning up /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/OpenCSM/trunk/pyOCSM
Deleting /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/OpenCSM/trunk/pyOCSM/pyOCSM/__pycache__
Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/pyOCSM at revision '2024-06-22T22:19:10.439 -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 2508
No changes for svn+ssh://acdl.mit.edu/home/svnroot/EGADS 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’
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/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 [reynolds] is in [[macys, macys_VM, reynolds, viggen]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[LINUX64] $ /bin/bash -xe /tmp/jenkins2075732443555322186.sh
+ rm -rf /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/training/lectures
+ [[ CAPS/LINEARAERO != *\S\l\u\g\s* ]]
+ rm -rf /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/OpenCSM/trunk/data/Slugs
+ [[ reynolds == *\v\i\g\g\e\n* ]]
+ bash -ex /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/JenkinsESP/ESP_Regression.sh
+ source /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.8
++ OCCTREF=7.8
++ AFLR_VERSION=11.5.14
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.38.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ export MPLBACKEND=agg
++ MPLBACKEND=agg
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ reynolds == \r\e\y\n\o\l\d\s ]]
++ [[ LINUX64 == \L\I\N\U\X\6\4\.\g\n\u* ]]
++ [[ LINUX64 == *\.\i\f\o\r\t ]]
++ '[' -f /opt/intel/oneapi/setvars.sh ']'
++ source /opt/intel/oneapi/setvars.sh
++ '[' -f /home/jenkins/.bashrc ']'
++ source /home/jenkins/.bashrc
+++ DEBUG_MODE=0
+++ [[ ehxB == *x* ]]
+++ DEBUG_MODE=1
+++ set +x
+++ case $- in
+++ return
++ export CAPS_OUTLEVEL=0
++ CAPS_OUTLEVEL=0
++ [[ LINUX64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64
++ ESP_BLOC=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64
++ export ESP_ROOT=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64
++ ESP_ROOT=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64
++ export JULIA_DEPOT_PATH=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/julia
++ JULIA_DEPOT_PATH=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.8 != '' ]]
++ [[ '' != '' ]]
++ [[ reynolds == *\r\e\y\n\o\l\d\s* ]]
++ [[ '' != '' ]]
++ [[ -d /home/jenkins/util/ESP/Python/ESP_Python-3.11.9 ]]
++ export PYTHONHOME=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9
++ PYTHONHOME=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9
++ export PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ export LD_LIBRARY_PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:/opt/intel/oneapi/tbb/2021.11/env/../lib/intel64/gcc4.8:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/lib:/opt/intel/oneapi/mpi/2021.11/lib:/opt/intel/oneapi/mkl/2024.0/lib:/opt/intel/oneapi/dpl/2022.3/lib:/opt/intel/oneapi/debugger/2024.0/opt/debugger/lib:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/host/linux64/lib:/opt/intel/oneapi/compiler/2024.0/opt/compiler/lib:/opt/intel/oneapi/compiler/2024.0/lib
++ LD_LIBRARY_PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:/opt/intel/oneapi/tbb/2021.11/env/../lib/intel64/gcc4.8:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/lib:/opt/intel/oneapi/mpi/2021.11/lib:/opt/intel/oneapi/mkl/2024.0/lib:/opt/intel/oneapi/dpl/2022.3/lib:/opt/intel/oneapi/debugger/2024.0/opt/debugger/lib:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/host/linux64/lib:/opt/intel/oneapi/compiler/2024.0/opt/compiler/lib:/opt/intel/oneapi/compiler/2024.0/lib
++ export EMPnumProc=4
++ EMPnumProc=4
++ export OMP_NUM_THREADS=4
++ OMP_NUM_THREADS=4
++ '[' '!' -z '' ']'
+++ ls -d /home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export CASARCH=.
++ CASARCH=.
++ export LD_LIBRARY_PATH=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:/opt/intel/oneapi/tbb/2021.11/env/../lib/intel64/gcc4.8:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/lib:/opt/intel/oneapi/mpi/2021.11/lib:/opt/intel/oneapi/mkl/2024.0/lib:/opt/intel/oneapi/dpl/2022.3/lib:/opt/intel/oneapi/debugger/2024.0/opt/debugger/lib:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/host/linux64/lib:/opt/intel/oneapi/compiler/2024.0/opt/compiler/lib:/opt/intel/oneapi/compiler/2024.0/lib
++ LD_LIBRARY_PATH=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:/opt/intel/oneapi/tbb/2021.11/env/../lib/intel64/gcc4.8:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/lib:/opt/intel/oneapi/mpi/2021.11/lib:/opt/intel/oneapi/mkl/2024.0/lib:/opt/intel/oneapi/dpl/2022.3/lib:/opt/intel/oneapi/debugger/2024.0/opt/debugger/lib:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/host/linux64/lib:/opt/intel/oneapi/compiler/2024.0/opt/compiler/lib:/opt/intel/oneapi/compiler/2024.0/lib
++ export ESP_EXTERN_LIBS=/home/jenkins/util/ESP/ExternLibs
++ ESP_EXTERN_LIBS=/home/jenkins/util/ESP/ExternLibs
++ export AFLR=/home/jenkins/util/AFLR/aflr_lib_11.5.14
++ AFLR=/home/jenkins/util/AFLR/aflr_lib_11.5.14
++ export AFLR_ARCH=Linux-x86-64
++ AFLR_ARCH=Linux-x86-64
++ export PATH=/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ PATH=/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ export CART3D=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16
++ CART3D=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16
++ export CART3D_ARCH=X86_64_ICC
++ CART3D_ARCH=X86_64_ICC
++ export PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ export PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ export PATH=/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ PATH=/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ export PATH=/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ PATH=/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ export MYSTRAN_directory=/home/jenkins/util/mystran/MYSTRAN/Binaries
++ MYSTRAN_directory=/home/jenkins/util/mystran/MYSTRAN/Binaries
++ export PATH=/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ PATH=/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ export PATH=/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ PATH=/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ export CAPS_GLYPH=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/pointwise/glyph
++ export PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ [[ reynolds == \r\e\y\n\o\l\d\s ]]
++ export SEACAS=/home/jenkins/util/sandialabs/seacas
++ SEACAS=/home/jenkins/util/sandialabs/seacas
++ export SU2_HOME=/home/jenkins/util/SU2/SU2-v8.0.0
++ SU2_HOME=/home/jenkins/util/SU2/SU2-v8.0.0
++ export SU2_RUN=/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ SU2_RUN=/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ export PATH=/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ '[' -d /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16 ']'
+++ perl -I/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/lib/perl5 -Mlocal::lib=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl
++ eval 'PATH="/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/bin${PATH:+:${PATH}}"; export PATH;
PERL5LIB="/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/lib/perl5${PERL5LIB:+:${PERL5LIB}}"; export PERL5LIB;
PERL_LOCAL_LIB_ROOT="/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl${PERL_LOCAL_LIB_ROOT:+:${PERL_LOCAL_LIB_ROOT}}"; export PERL_LOCAL_LIB_ROOT;
PERL_MB_OPT="--install_base \"/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl\""; export PERL_MB_OPT;
PERL_MM_OPT="INSTALL_BASE=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl"; export PERL_MM_OPT;'
+++ PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
+++ export PATH
+++ PERL5LIB=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/lib/perl5
+++ export PERL5LIB
+++ PERL_LOCAL_LIB_ROOT=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl
+++ export PERL_LOCAL_LIB_ROOT
+++ PERL_MB_OPT='--install_base "/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl"'
+++ export PERL_MB_OPT
+++ PERL_MM_OPT=INSTALL_BASE=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl
+++ export PERL_MM_OPT
++ export PATH=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test:/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test:/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/OpenCSM/trunk/pyOCSM:/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/OpenCSM/trunk/pyOCSM:/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/pyCAPS:/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/OpenCSM/trunk/pyOCSM:/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/pyCAPS:/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/OpenCSM/trunk/pyOCSM:/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ [[ reynolds == \m\a\c\y\s* ]]
++ [[ reynolds == \v\i\g\g\e\n ]]
+++ python-config --includes
++ export 'PYTHONINC=. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
++ PYTHONINC='. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
+++ python-config --help
++ [[ Usage: /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python-config --prefix|--exec-prefix|--includes|--libs|--cflags|--ldflags|--extension-suffix|--help|--abiflags|--configdir|--embed == *\e\m\b\e\d* ]]
+++ python-config --ldflags --embed
++ export 'PYTHONLIB= -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lpthread -ldl -lutil -lm '
++ PYTHONLIB=' -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lpthread -ldl -lutil -lm '
++ [[ reynolds == \m\a\c\y\s ]]
++ [[ reynolds == \v\i\g\g\e\n ]]
++ export PYTHONUNBUFFERED=true
++ PYTHONUNBUFFERED=true
++ export PYTHONFAULTHANDLER=true
++ PYTHONFAULTHANDLER=true
++ python --version
Python 3.11.9
++ [[ LINUX64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export CSMDATA=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/OpenCSM/trunk/data
++ CSMDATA=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/OpenCSM/trunk/data
+ source /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/JenkinsESP/ESPbfr.sh
++ cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/
++ tar -xvf /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/JenkinsESP/ESPbfr.tgz
ESP/
ESP/CYGWIN64/
ESP/CYGWIN64/bin/
ESP/CYGWIN64/bin/mastros.exe
ESP/CYGWIN64/bin/ASTRO.D01
ESP/CYGWIN64/bin/ASTRO.IDX
ESP/CYGWIN64/include/
ESP/CYGWIN64/lib/
ESP/CYGWIN64/lib/libquadmath-0.dll
ESP/CYGWIN64/lib/libwinpthread-1.dll
ESP/CYGWIN64/lib/libgcc_s_sjlj-1.dll
ESP/CYGWIN64/obj/
ESP/CYGWIN64/test/
ESP/DARWIN64/
ESP/DARWIN64/bin/
ESP/DARWIN64/bin/mastros.exe
ESP/DARWIN64/bin/ASTRO.D01
ESP/DARWIN64/bin/mset
ESP/DARWIN64/bin/ASTRO.IDX
ESP/DARWIN64/bin/avl
ESP/DARWIN64/bin/xfoil
ESP/DARWIN64/bin/mses
ESP/DARWIN64/include/
ESP/DARWIN64/include/nmb.h
ESP/DARWIN64/include/xddm/
ESP/DARWIN64/include/xddm/xddmInternals.h
ESP/DARWIN64/include/xddm/xddm.h
ESP/DARWIN64/include/xddm/xddm.c
ESP/DARWIN64/include/converter.h
ESP/DARWIN64/include/libCart3D/
ESP/DARWIN64/include/libCart3D/sensors.h
ESP/DARWIN64/include/libCart3D/SFC.h
ESP/DARWIN64/include/libCart3D/map.h
ESP/DARWIN64/include/libCart3D/MGinfo.h
ESP/DARWIN64/include/libCart3D/gridStructures.h
ESP/DARWIN64/include/libCart3D/timer.h
ESP/DARWIN64/include/libCart3D/ConvInfo.h
ESP/DARWIN64/include/libCart3D/dualtime.h
ESP/DARWIN64/include/libCart3D/stateVector.h
ESP/DARWIN64/include/libCart3D/cartCells.h
ESP/DARWIN64/include/libCart3D/encoding.h
ESP/DARWIN64/include/libCart3D/string_util.h
ESP/DARWIN64/include/libCart3D/int64.h
ESP/DARWIN64/include/libCart3D/bBox_stuff.h
ESP/DARWIN64/include/libCart3D/basicTypes.h
ESP/DARWIN64/include/libCart3D/utils_xml.h
ESP/DARWIN64/include/libCart3D/hex.h
ESP/DARWIN64/include/libCart3D/PostProcInfo.h
ESP/DARWIN64/include/libCart3D/SolverInfo.h
ESP/DARWIN64/include/libCart3D/earthBL_BC.h
ESP/DARWIN64/include/libCart3D/limiters.h
ESP/DARWIN64/include/libCart3D/geomStructures.h
ESP/DARWIN64/include/libCart3D/CaseInfo.h
ESP/DARWIN64/include/libCart3D/memory_util.h
ESP/DARWIN64/include/libCart3D/infoStructures.h
ESP/DARWIN64/include/libCart3D/geomTypes.h
ESP/DARWIN64/include/libCart3D/c3d_timeout.h
ESP/DARWIN64/include/libCart3D/myLList.h
ESP/DARWIN64/include/libCart3D/IOinfo.h
ESP/DARWIN64/include/libCart3D/GridInfo.h
ESP/DARWIN64/include/libCart3D/c3d_global.h
ESP/DARWIN64/include/libCart3D/vortexBC.h
ESP/DARWIN64/include/c3dio/
ESP/DARWIN64/include/c3dio/c3dio_icemcfd.h
ESP/DARWIN64/include/c3dio/c3dio_lib.h
ESP/DARWIN64/include/udunits.h
ESP/DARWIN64/include/udunits2.h
ESP/DARWIN64/lib/
ESP/DARWIN64/lib/libudunits2.dylib
ESP/DARWIN64/lib/libudunits2.0.dylib
ESP/DARWIN64/lib/libCart3D.a
ESP/DARWIN64/lib/libnmb.dylib
ESP/DARWIN64/lib/libc3dio.a
ESP/DARWIN64/obj/
ESP/DARWIN64/test/
ESP/DARWIN_ARM64/
ESP/DARWIN_ARM64/bin/
ESP/DARWIN_ARM64/bin/mastros.exe
ESP/DARWIN_ARM64/bin/ASTRO.D01
ESP/DARWIN_ARM64/bin/mset
ESP/DARWIN_ARM64/bin/ASTRO.IDX
ESP/DARWIN_ARM64/bin/avl
ESP/DARWIN_ARM64/bin/xfoil
ESP/DARWIN_ARM64/bin/mses
ESP/DARWIN_ARM64/include/
ESP/DARWIN_ARM64/include/nmb.h
ESP/DARWIN_ARM64/include/xddm/
ESP/DARWIN_ARM64/include/xddm/xddmInternals.h
ESP/DARWIN_ARM64/include/xddm/xddm.h
ESP/DARWIN_ARM64/include/xddm/xddm.c
ESP/DARWIN_ARM64/include/converter.h
ESP/DARWIN_ARM64/include/libCart3D/
ESP/DARWIN_ARM64/include/libCart3D/sensors.h
ESP/DARWIN_ARM64/include/libCart3D/SFC.h
ESP/DARWIN_ARM64/include/libCart3D/map.h
ESP/DARWIN_ARM64/include/libCart3D/MGinfo.h
ESP/DARWIN_ARM64/include/libCart3D/gridStructures.h
ESP/DARWIN_ARM64/include/libCart3D/timer.h
ESP/DARWIN_ARM64/include/libCart3D/ConvInfo.h
ESP/DARWIN_ARM64/include/libCart3D/dualtime.h
ESP/DARWIN_ARM64/include/libCart3D/stateVector.h
ESP/DARWIN_ARM64/include/libCart3D/cartCells.h
ESP/DARWIN_ARM64/include/libCart3D/encoding.h
ESP/DARWIN_ARM64/include/libCart3D/string_util.h
ESP/DARWIN_ARM64/include/libCart3D/int64.h
ESP/DARWIN_ARM64/include/libCart3D/bBox_stuff.h
ESP/DARWIN_ARM64/include/libCart3D/basicTypes.h
ESP/DARWIN_ARM64/include/libCart3D/utils_xml.h
ESP/DARWIN_ARM64/include/libCart3D/hex.h
ESP/DARWIN_ARM64/include/libCart3D/PostProcInfo.h
ESP/DARWIN_ARM64/include/libCart3D/SolverInfo.h
ESP/DARWIN_ARM64/include/libCart3D/earthBL_BC.h
ESP/DARWIN_ARM64/include/libCart3D/limiters.h
ESP/DARWIN_ARM64/include/libCart3D/geomStructures.h
ESP/DARWIN_ARM64/include/libCart3D/CaseInfo.h
ESP/DARWIN_ARM64/include/libCart3D/memory_util.h
ESP/DARWIN_ARM64/include/libCart3D/infoStructures.h
ESP/DARWIN_ARM64/include/libCart3D/geomTypes.h
ESP/DARWIN_ARM64/include/libCart3D/c3d_timeout.h
ESP/DARWIN_ARM64/include/libCart3D/myLList.h
ESP/DARWIN_ARM64/include/libCart3D/IOinfo.h
ESP/DARWIN_ARM64/include/libCart3D/GridInfo.h
ESP/DARWIN_ARM64/include/libCart3D/c3d_global.h
ESP/DARWIN_ARM64/include/libCart3D/vortexBC.h
ESP/DARWIN_ARM64/include/c3dio/
ESP/DARWIN_ARM64/include/c3dio/c3dio_icemcfd.h
ESP/DARWIN_ARM64/include/c3dio/c3dio_lib.h
ESP/DARWIN_ARM64/include/udunits.h
ESP/DARWIN_ARM64/include/udunits2.h
ESP/DARWIN_ARM64/lib/
ESP/DARWIN_ARM64/lib/libudunits2.dylib
ESP/DARWIN_ARM64/lib/libudunits2.0.dylib
ESP/DARWIN_ARM64/lib/libCart3D.a
ESP/DARWIN_ARM64/lib/libc3dio.a
ESP/DARWIN_ARM64/obj/
ESP/DARWIN_ARM64/test/
ESP/LINUX64/
ESP/LINUX64/bin/
ESP/LINUX64/bin/mastros.exe
ESP/LINUX64/bin/ASTRO.D01
ESP/LINUX64/bin/mset
ESP/LINUX64/bin/ASTRO.IDX
ESP/LINUX64/bin/avl
ESP/LINUX64/bin/xfoil
ESP/LINUX64/bin/mses
ESP/LINUX64/include/
ESP/LINUX64/include/nmb.h
ESP/LINUX64/include/xddm/
ESP/LINUX64/include/xddm/xddmInternals.h
ESP/LINUX64/include/xddm/xddm.h
ESP/LINUX64/include/xddm/xddm.c
ESP/LINUX64/include/libCart3D/
ESP/LINUX64/include/libCart3D/sensors.h
ESP/LINUX64/include/libCart3D/SFC.h
ESP/LINUX64/include/libCart3D/map.h
ESP/LINUX64/include/libCart3D/MGinfo.h
ESP/LINUX64/include/libCart3D/gridStructures.h
ESP/LINUX64/include/libCart3D/timer.h
ESP/LINUX64/include/libCart3D/ConvInfo.h
ESP/LINUX64/include/libCart3D/dualtime.h
ESP/LINUX64/include/libCart3D/stateVector.h
ESP/LINUX64/include/libCart3D/cartCells.h
ESP/LINUX64/include/libCart3D/encoding.h
ESP/LINUX64/include/libCart3D/string_util.h
ESP/LINUX64/include/libCart3D/int64.h
ESP/LINUX64/include/libCart3D/bBox_stuff.h
ESP/LINUX64/include/libCart3D/basicTypes.h
ESP/LINUX64/include/libCart3D/utils_xml.h
ESP/LINUX64/include/libCart3D/hex.h
ESP/LINUX64/include/libCart3D/PostProcInfo.h
ESP/LINUX64/include/libCart3D/SolverInfo.h
ESP/LINUX64/include/libCart3D/earthBL_BC.h
ESP/LINUX64/include/libCart3D/limiters.h
ESP/LINUX64/include/libCart3D/geomStructures.h
ESP/LINUX64/include/libCart3D/CaseInfo.h
ESP/LINUX64/include/libCart3D/memory_util.h
ESP/LINUX64/include/libCart3D/infoStructures.h
ESP/LINUX64/include/libCart3D/geomTypes.h
ESP/LINUX64/include/libCart3D/c3d_timeout.h
ESP/LINUX64/include/libCart3D/myLList.h
ESP/LINUX64/include/libCart3D/IOinfo.h
ESP/LINUX64/include/libCart3D/GridInfo.h
ESP/LINUX64/include/libCart3D/c3d_global.h
ESP/LINUX64/include/libCart3D/vortexBC.h
ESP/LINUX64/include/c3dio/
ESP/LINUX64/include/c3dio/c3dio_icemcfd.h
ESP/LINUX64/include/c3dio/c3dio_lib.h
ESP/LINUX64/lib/
ESP/LINUX64/lib/libnmb.so
ESP/LINUX64/lib/libCart3D.a
ESP/LINUX64/lib/libc3dio.a
ESP/LINUX64/obj/
ESP/LINUX64/test/
ESP/WIN64/
ESP/WIN64/bin/
ESP/WIN64/bin/mses.exe
ESP/WIN64/bin/avl.exe
ESP/WIN64/bin/mastros.exe
ESP/WIN64/bin/ASTRO.D01
ESP/WIN64/bin/xfoil.exe
ESP/WIN64/bin/ASTRO.IDX
ESP/WIN64/bin/mset.exe
ESP/WIN64/include/
ESP/WIN64/include/nmb.h
ESP/WIN64/include/winhelpers/
ESP/WIN64/include/winhelpers/gettimeofday.h
ESP/WIN64/include/winhelpers/websock-w32.h
ESP/WIN64/include/winhelpers/netdb.h
ESP/WIN64/include/winhelpers/unistd.h
ESP/WIN64/include/winhelpers/strings.h
ESP/WIN64/include/winhelpers/sys/
ESP/WIN64/include/winhelpers/sys/time.h
ESP/WIN64/include/converter.h
ESP/WIN64/include/udunits.h
ESP/WIN64/include/udunits2.h
ESP/WIN64/lib/
ESP/WIN64/lib/libquadmath-0.dll
ESP/WIN64/lib/nmb.lib
ESP/WIN64/lib/libwinpthread-1.dll
ESP/WIN64/lib/udunits2.lib
ESP/WIN64/lib/libgcc_s_sjlj-1.dll
ESP/WIN64/lib/expat.dll
ESP/WIN64/lib/udunits2.dll
ESP/WIN64/lib/nmb.dll
ESP/WIN64/obj/
ESP/WIN64/test/
ESP/LINUX_AARCH64/
ESP/LINUX_AARCH64/bin/
ESP/LINUX_AARCH64/bin/mastros.exe
ESP/LINUX_AARCH64/bin/ASTRO.D01
ESP/LINUX_AARCH64/bin/mset
ESP/LINUX_AARCH64/bin/ASTRO.IDX
ESP/LINUX_AARCH64/bin/avl
ESP/LINUX_AARCH64/bin/xfoil
ESP/LINUX_AARCH64/bin/mses
ESP/LINUX_AARCH64/include/
ESP/LINUX_AARCH64/lib/
ESP/LINUX_AARCH64/obj/
ESP/LINUX_AARCH64/test/
ESP/udunits/
ESP/udunits/udunits2-accepted.xml
ESP/udunits/udunits2-base.xml
ESP/udunits/udunits2-common.xml
ESP/udunits/udunits2.xml
ESP/udunits/udunits2-derived.xml
ESP/udunits/udunits2-prefixes.xml
++ virtualenv --system-site-packages /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/venv
created virtual environment CPython3.11.9.final.0-64 in 161ms
creator CPython3Posix(dest=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/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=/home/jenkins/.local/share/virtualenv)
added seed packages: pip==24.0, setuptools==70.0.0, wheel==0.43.0
activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator
++ . /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/venv/bin/activate
+++ '[' /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/venv/bin/activate = /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/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=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/venv
+++ '[' linux-gnu = cygwin ']'
+++ '[' linux-gnu = msys ']'
+++ export VIRTUAL_ENV
+++ _OLD_VIRTUAL_PATH=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test:/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
+++ PATH=/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/venv/bin:/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test:/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
+++ export PATH
+++ '[' x '!=' x ']'
++++ basename /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/venv
+++ VIRTUAL_ENV_PROMPT=venv
+++ export VIRTUAL_ENV_PROMPT
+++ '[' -z _ ']'
+++ _OLD_VIRTUAL_PYTHONHOME=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9
+++ unset PYTHONHOME
+++ '[' -z '' ']'
+++ _OLD_VIRTUAL_PS1=
+++ PS1='(venv) '
+++ export PS1
+++ alias pydoc
+++ true
+++ hash -r
++ pip_install pip
++ /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/venv/bin/python -m pip install --only-binary all --upgrade pip
Requirement already satisfied: pip in ./ESP/venv/lib/python3.11/site-packages (24.0)
Collecting pip
Using cached pip-24.1-py3-none-any.whl.metadata (3.6 kB)
Using cached pip-24.1-py3-none-any.whl (1.8 MB)
Installing collected packages: pip
Attempting uninstall: pip
Found existing installation: pip 24.0
Uninstalling pip-24.0:
Successfully uninstalled pip-24.0
Successfully installed pip-24.1
++ pip_install f90nml
++ /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/venv/bin/python -m pip install --only-binary all --upgrade f90nml
Requirement already satisfied: f90nml in /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (1.4.4)
++ pip_install numpy
++ /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/venv/bin/python -m pip install --only-binary all --upgrade numpy
Requirement already satisfied: numpy in /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (1.26.4)
Collecting numpy
Using cached numpy-2.0.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (60 kB)
Using cached numpy-2.0.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (19.3 MB)
Installing collected packages: numpy
Attempting uninstall: numpy
Found existing installation: numpy 1.26.4
Not uninstalling numpy at /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages, outside environment /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/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.
pynastran 1.4.1 requires numpy<2, but you have numpy 2.0.0 which is incompatible.
tacs 3.7.2 requires numpy<2.0.0, but you have numpy 2.0.0 which is incompatible.
numba 0.59.1 requires numpy<1.27,>=1.22, but you have numpy 2.0.0 which is incompatible.
openmdao 3.33.0 requires numpy<2, but you have numpy 2.0.0 which is incompatible.
Successfully installed numpy-2.0.0
++ pip_install 'scipy!=1.9.2,!=1.9.3'
++ /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/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 /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (1.13.1)
Requirement already satisfied: numpy<2.3,>=1.22.4 in ./ESP/venv/lib/python3.11/site-packages (from scipy!=1.9.2,!=1.9.3) (2.0.0)
++ pip_install openmdao
++ /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/venv/bin/python -m pip install --only-binary all --upgrade openmdao
Requirement already satisfied: openmdao in /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (3.33.0)
Requirement already satisfied: networkx>=2.0 in /home/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-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (61 kB)
Requirement already satisfied: packaging in /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from openmdao) (24.0)
Requirement already satisfied: requests in /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from openmdao) (2.32.3)
Requirement already satisfied: scipy in /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from openmdao) (1.13.1)
Requirement already satisfied: charset-normalizer<4,>=2 in /home/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 /home/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 /home/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 /home/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-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (18.3 MB)
Installing collected packages: numpy
Attempting uninstall: numpy
Found existing installation: numpy 2.0.0
Uninstalling numpy-2.0.0:
Successfully uninstalled numpy-2.0.0
Successfully installed numpy-1.26.4
++ [[ reynolds == *\v\i\g\g\e\n* ]]
++ pip_install cvxopt
++ /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/venv/bin/python -m pip install --only-binary all --upgrade cvxopt
Requirement already satisfied: cvxopt in /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (1.3.2)
++ pip_install dill
++ /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/venv/bin/python -m pip install --only-binary all --upgrade dill
Requirement already satisfied: dill in /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (0.3.8)
++ pip_install packaging
++ /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/venv/bin/python -m pip install --only-binary all --upgrade packaging
Requirement already satisfied: packaging in /home/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 /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages, outside environment /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/venv
Can't uninstall 'packaging'. No files were found to uninstall.
Successfully installed packaging-24.1
++ pip_install matplotlib
++ /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/venv/bin/python -m pip install --only-binary all --upgrade matplotlib
Requirement already satisfied: matplotlib in /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (3.9.0)
Requirement already satisfied: contourpy>=1.0.1 in /home/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 /home/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 /home/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 /home/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 /home/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 /home/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 /home/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 /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from python-dateutil>=2.7->matplotlib) (1.16.0)
++ [[ /home/jenkins/util/ESP/ExternLibs == '' ]]
++ '[' -d /home/jenkins/util/ESP/ExternLibs ']'
++ cp /home/jenkins/util/ESP/ExternLibs/intersectWake.so /home/jenkins/util/ESP/ExternLibs/markWakeEdges.so /home/jenkins/util/ESP/ExternLibs/sansLIPAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/
++ cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/EGADS/trunk/src
++ make
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/LINUX64
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/LINUX64
cp -p ../include/LINUX64 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/LINUX64
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/STANALYZER.make
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/STANALYZER.make
cp -p ../include/STANALYZER.make /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/STANALYZER.make
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egads.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egads.h
cp -p ../include/egads.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egads.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egads_dot.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egads_dot.h
cp -p ../include/egads_dot.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egads_dot.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egads.inc
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egads.inc
cp -p ../include/egads.inc /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egads.inc
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egadsErrors.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egadsErrors.h
cp -p ../include/egadsErrors.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egadsErrors.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egadsTypes.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egadsTypes.h
cp -p ../include/egadsTypes.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egadsTypes.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/emp.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/emp.h
cp -p ../include/emp.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/emp.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/prm.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/prm.h
cp -p ../include/prm.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/prm.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/wsserver.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/wsserver.h
cp -p ../include/wsserver.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/wsserver.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/wsserver.inc
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/wsserver.inc
cp -p ../include/wsserver.inc /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/wsserver.inc
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/wsss.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/wsss.h
cp -p ../include/wsss.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/wsss.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egadsTris.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egadsTris.h
cp -p egadsTris.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egadsTris.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egadsSplineFit.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egadsSplineFit.h
cp -p egadsSplineFit.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egadsSplineFit.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egadsSplineVels.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egadsSplineVels.h
cp -p egadsSplineVels.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egadsSplineVels.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egadsf90.inc
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egadsf90.inc
cp -p ../include/egadsf90.inc /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egadsf90.inc
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/Surreal
cp Surreal/SurrealD.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/Surreal/SurrealD.h
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/Surreal
cp Surreal/SurrealD_Lazy.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/Surreal/SurrealD_Lazy.h
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/Surreal
cp Surreal/SurrealD_Trad.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/Surreal/SurrealD_Trad.h
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/Surreal
cp Surreal/SurrealS.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/Surreal/SurrealS.h
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/Surreal
cp Surreal/SurrealS_Lazy.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/Surreal/SurrealS_Lazy.h
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/Surreal
cp Surreal/SurrealS_Trad.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/Surreal/SurrealS_Trad.h
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/Surreal
cp Surreal/always_inline.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/Surreal/always_inline.h
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsGeom.cpp -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsGeom.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsHLevel.cpp -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsHLevel.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsTopo.cpp -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsTopo.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsCopy.cpp -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsCopy.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsSpline.cpp -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsSpline.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsIO.cpp -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsIO.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsSplineFit.cpp -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsSplineFit.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsSkinning.cpp -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsSkinning.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsTessSens.cpp -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsTessSens.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 OCC/BRepLib_FuseEdges.cpp -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/BRepLib_FuseEdges.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsBase.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsBase.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsMemory.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsMemory.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsAttrs.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsAttrs.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsTess.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsTess.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsTessInp.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsTessInp.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsTris.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsTris.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsQuads.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsQuads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsFit.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsFit.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsRobust.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsRobust.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsSBO.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsSBO.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap prmCfit.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/prmCfit.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap prmGrid.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/prmGrid.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap prmUV.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/prmUV.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsExport.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsExport.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsEffect.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsEffect.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsSolids.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsSolids.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include ../util/emp.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/emp.o
g++ -g -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \
../util/evaluate.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/evaluate.o
g++ -g -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \
../util/rational.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/rational.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include -I../util \
../util/regQuads.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/regQuads.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/SurrealD1
SurrealD1_test_suite Complete!
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/SurrealD4 -O -std=c++11 -I. ../util/SurrealD4_btest.cpp
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/SurrealD4
SurrealD4_test_suite Complete!
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/SurrealS1 -O -std=c++11 -I. ../util/SurrealS1_btest.cpp
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/SurrealS1
SurrealS1_test_suite Complete!
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/SurrealS4 -O -std=c++11 -I. ../util/SurrealS4_btest.cpp
../util/SurrealS4_btest.cpp: In function ‘void multiply_deriv2()’:
../util/SurrealS4_btest.cpp:1265:23: note: variable tracking size limit exceeded with ‘-fvar-tracking-assignments’, retrying without
1265 | BOOST_AUTO_TEST_CASE( multiply_deriv2 )
| ^~~~~~~~~~~~~~~
../util/SurrealS4_btest.cpp:19:42: note: in definition of macro ‘BOOST_AUTO_TEST_CASE’
19 | #define BOOST_AUTO_TEST_CASE( fun ) void fun()
| ^~~
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/SurrealS4
SurrealS4_test_suite Complete!
make -C ../util
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/EGADS/trunk/util'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 uvmap/main/uvmap.c -Iuvmap \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapFindUV.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/EG_uvmapFindUV.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapGen.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/EG_uvmapGen.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmap_Read.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/EG_uvmap_Read.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapStructFree.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/EG_uvmapStructFree.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapTest.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/EG_uvmapTest.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmap_Write.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/EG_uvmap_Write.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_add.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_add.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_bnd_adj.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_bnd_adj.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_chk_area_uv.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_chk_area_uv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_chk_edge_ratio.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_chk_edge_ratio.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_cpu_message.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_cpu_message.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_find_uv.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_find_uv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_from_egads.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_from_egads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_gen.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_gen.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_gen_uv.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_gen_uv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibeibe.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_ibeibe.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibfibf.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_ibfibf.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibfin.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_ibfin.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_iccibe.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_iccibe.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_iccin.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_iccin.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_idibe.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_idibe.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_inibe.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_inibe.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_inl_uv_bnd.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_inl_uv_bnd.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_malloc.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_malloc.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_mben_disc.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_mben_disc.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_message.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_message.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_norm_uv.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_norm_uv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_read.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_read.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_solve.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_solve.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_struct_tasks.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_struct_tasks.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_test.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_test.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_to_egads.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_to_egads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_version.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_version.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_write.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap_write.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 egadsUVmap.c -Iuvmap \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsUVmap.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libuvmap.a
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libuvmap.a
(cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj; ar rs /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libuvmap.a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsUVmap.o EG_uvmapFindUV.o EG_uvmapGen.o EG_uvmap_Read.o EG_uvmapStructFree.o EG_uvmapTest.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 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libuvmap.a
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/uvmap.exe /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/uvmap.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -luvmap -lrt -lm
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/EGADS/trunk/util'
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libegads.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libegads.so
(cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj; gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libegads.so \
egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o emp.o evaluate.o rational.o regQuads.o \
-L/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -pthread -lm -lstdc++ -lrt )
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libegadstatic.a
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libegadstatic.a
cp /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libuvmap.a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libegadstatic.a
(cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj; \
ar rs /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libegadstatic.a egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o emp.o \
evaluate.o rational.o regQuads.o; )
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsBase.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fgadsBase.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsMemory.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fgadsMemory.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsAttrs.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fgadsAttrs.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsTess.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fgadsTess.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsHLevel.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fgadsHLevel.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsGeom.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fgadsGeom.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsTopo.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fgadsTopo.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libfgads.a
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libfgads.a
(cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj; ar rs /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libfgads.a fgadsBase.o fgadsMemory.o fgadsAttrs.o fgadsTess.o fgadsHLevel.o fgadsGeom.o fgadsTopo.o; )
ar: creating /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libfgads.a
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libemp.a
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libemp.a
(cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj; ar rs /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libemp.a emp.o; )
ar: creating /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libemp.a
*** EGADS Build Complete! ***
++ cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/EGADS/trunk/wvServer
++ make
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 map.cpp -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/map.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include base64-decode.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/base64-decode.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include handshake.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/handshake.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include client-handshake.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/client-handshake.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include libwebsockets.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/libwebsockets.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include extension-deflate-stream.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/extension-deflate-stream.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include md5.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/md5.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include extension-x-google-mux.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/extension-x-google-mux.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include parsers.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/parsers.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include extension.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/extension.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include sha-1.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/sha-1.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include server.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/server.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include wv.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/wv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include browserMessage.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/browserMessage.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include fwv.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fwv.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libwsserver.a
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libwsserver.a
(cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj; ar rs /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/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 \
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fwv.o; )
ar: creating /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libwsserver.a
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -DSTANDALONE server.c \
-I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/servertest.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/server /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/servertest.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libwsserver.a \
-lpthread -lz -lm
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libwsserver.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libwsserver.so
(cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj; g++ -g -shared -Wl,-no-undefined \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libwsserver.so base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o map.o -lz -lpthread)
++ cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/EGADS/trunk/lite
++ make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteBase.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/liteBase.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteMemory.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/liteMemory.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteGeom.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/liteGeom.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteTopo.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/liteTopo.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteAttrs.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/liteAttrs.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteImport.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/liteImport.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteString.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/liteString.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../src/egadsTess.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/liteTess.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../src/egadsTris.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/liteTris.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src \
../src/egadsQuads.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/liteQuads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
-I../util ../src/egadsTessInp.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/liteTessInp.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../util/evaluate.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/evaLite.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE ../util/rational.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/ratLite.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I../util \
../util/regQuads.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/liteRegQuads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../src/egadsEffect.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/liteEffect.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
-I../util/uvmap liteUVmap.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/liteUVmap.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libegadslite.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libegadslite.so
(cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj; gcc -g -shared -Wl,-no-undefined \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libegadslite.so liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o liteTess.o liteTris.o \
liteQuads.o liteTessInp.o egadsRobust.o emp.o evaLite.o \
ratLite.o liteRegQuads.o liteEffect.o liteUVmap.o \
-lpthread -lm )
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libegadslitestatic.a
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libegadslitestatic.a
(cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj; ar rs /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/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 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libegadslitestatic.a
++ cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/EGADS/trunk/test
+++ ls addKnots.make agglom.make approx.make blend.make BSplineIGES.make chamfer.make closure.make CSys.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 GBO.make globalTess.make hollowFace.make hollow.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 SBO.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 vTessInp.make vTess.make xform.make
++ for file in `ls *.make`
++ make -f addKnots.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include addKnots.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/addKnots.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/addKnots /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/addKnots.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f agglom.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include agglom.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/agglom.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/agglom /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/agglom.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lrt -legads -lm
++ for file in `ls *.make`
++ make -f approx.make
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include approx.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/approx.o
gfortran -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/approx /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/approx.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lfgads \
-legads -lstdc++
++ for file in `ls *.make`
++ make -f blend.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include blend.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/blend.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/blend /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/blend.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f BSplineIGES.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include BSplineIGES.c -o \
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/BSplineIGES.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/BSplineIGES /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/BSplineIGES.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f chamfer.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include chamfer.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/chamfer.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/chamfer /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/chamfer.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f closure.make
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include closure.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/closure.o
gfortran -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/closure /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/closure.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lfgads \
-legads -lstdc++
++ for file in `ls *.make`
++ make -f CSys.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include CSys.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/CSys.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/CSys /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/CSys.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f edge2WB.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include edge2WB.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/edge2WB.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/edge2WB /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/edge2WB.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f edges.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include edges.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/edges.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/edges /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/edges.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f effective.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include effective.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/effective.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/effective /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/effective.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f egads2cart.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include egads2cart.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads2cart.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/egads2cart /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads2cart.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f egads2ply.make
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. egads2ply.cpp -std=c++11 \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads2ply.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I. tinyply.cpp -std=c++11 -w \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/tinyply.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/egads2ply /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads2ply.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/tinyply.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f egadsGeom_dot.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include egadsGeom_dot.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsGeom_dot.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include egadsTools_dot.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsTools_dot.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/egadsGeom_dot /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsGeom_dot.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsTools_dot.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f egadsHLevel_dot.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include egadsHLevel_dot.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsHLevel_dot.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/egadsHLevel_dot /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsHLevel_dot.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsTools_dot.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f egadsSpline_dot.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include egadsSpline_dot.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsSpline_dot.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/egadsSpline_dot /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsSpline_dot.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsTools_dot.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f egadsTopo_dot.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include egadsTopo_dot.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsTopo_dot.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/egadsTopo_dot /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsTopo_dot.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsTools_dot.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f exportLite.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../util/uvmap \
../src/egadsExport.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/exportLite.o -DSTANDALONE
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/exportLite /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/exportLite.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f extrot.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include extrot.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/extrot.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/extrot /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/extrot.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f fillet.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include fillet.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fillet.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/fillet /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fillet.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f fit.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include fit.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fit.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/fit /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fit.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f fitTri.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include fitTri.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fitTri.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/fitTri /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fitTri.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f fullAttr.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include fullAttr.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fullAttr.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/fullAttr /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fullAttr.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f fuseSheets.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include fuseSheets.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fuseSheets.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/fuseSheets /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fuseSheets.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f GBO.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include GBO.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/GBO.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/GBO /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/GBO.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f globalTess.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include globalTess.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/globalTess.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/globalTess /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/globalTess.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f hollowFace.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include hollowFace.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hollowFace.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/hollowFace /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hollowFace.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f hollow.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include hollow.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hollow.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/hollow /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hollow.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f intersect.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include intersect.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/intersect.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/intersect /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/intersect.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f makeCone.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include makeCone.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/makeCone.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/makeCone /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/makeCone.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f makeFace3D.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include makeFace3D.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/makeFace3D.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/makeFace3D /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/makeFace3D.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f makeLoop.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include makeLoop.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/makeLoop.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/makeLoop /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/makeLoop.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f mapTess.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include mapTess.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/mapTess.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/mapTess /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/mapTess.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f mofb.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include mofb.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/mofb.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/mofb /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/mofb.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f mssb.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include mssb.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/mssb.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/mssb /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/mssb.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f multiContext.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include multiContext.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/multiContext.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/multiContext /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/multiContext.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib \
-legads -lrt -lm
++ for file in `ls *.make`
++ make -f offset.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include offset.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/offset.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/offset /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/offset.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f rebuild.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include rebuild.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/rebuild.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/rebuild /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/rebuild.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f refObj.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include refObj.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/refObj.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/refObj /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/refObj.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f replace.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include replace.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/replace.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/replace /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/replace.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f revolve.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include revolve.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/revolve.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/revolve /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/revolve.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f ruled.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include ruled.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/ruled.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/ruled /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/ruled.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f saveTess.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include saveTess.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/saveTess.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/saveTess /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/saveTess.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f SBO.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include SBO.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/SBO.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/SBO /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/SBO.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f scribe.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include scribe.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/scribe.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/scribe /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/scribe.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f sew.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include sew.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/sew.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/sew /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/sew.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f simplePer.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include simplePer.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/simplePer.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/simplePer /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/simplePer.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f smallEdges.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include smallEdges.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/smallEdges.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/smallEdges /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/smallEdges.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f step.make
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include step.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/step.o
gfortran -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/step /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/step.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lfgads -legads \
-lstdc++
++ for file in `ls *.make`
++ make -f sweep.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include sweep.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/sweep.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/sweep /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/sweep.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ for file in `ls *.make`
++ make -f test.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include testc.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/testc.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/testc /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/testc.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include testf.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/testf.o
gfortran -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/testf /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/testf.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lfgads -legads \
-lstdc++
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include parsec.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/parsec.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/parsec /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/parsec.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include parsef.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/parsef.o
gfortran -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/parsef /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/parsef.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lfgads -legads \
-lstdc++
++ for file in `ls *.make`
++ make -f tolerance.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include tolerance.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/tolerance.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/tolerance /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/tolerance.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lrt -lm
++ for file in `ls *.make`
++ make -f union.make
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include union.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/union.o
gfortran -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/union /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/union.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lfgads -legads \
-lstdc++
++ for file in `ls *.make`
++ make -f vAttr.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include vAttr.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vAttr.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/vAttr /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vAttr.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lwsserver -legads -lrt
++ for file in `ls *.make`
++ make -f vCurvature.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include vCurvature.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vCurvature.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/vCurvature /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vCurvature.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lwsserver -legads -lrt
++ for file in `ls *.make`
++ make -f vEffect.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include vEffect.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vEffect.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/vEffect /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vEffect.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lwsserver -legads -lrt
++ for file in `ls *.make`
++ make -f vEto.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include vEto.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vEto.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/vEto /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vEto.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lwsserver -lrt
++ for file in `ls *.make`
++ make -f vFrame.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include vFrame.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vFrame.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/vFrame /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vFrame.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lwsserver -lrt
++ for file in `ls *.make`
++ make -f vGeom.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include vGeom.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vGeom.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/vGeom /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vGeom.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lwsserver -legads \
-lrt
++ for file in `ls *.make`
++ make -f vQuad.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include vQuad.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vQuad.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/vQuad /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vQuad.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lwsserver \
-legads -lrt
++ for file in `ls *.make`
++ make -f vTessInp.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include vTessInp.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vTessInp.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/vTessInp /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vTessInp.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lwsserver -legads -lrt
++ for file in `ls *.make`
++ make -f vTess.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include vTess.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vTess.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include ../util/retessFaces.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/retessFaces.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/vTesstatic /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vTess.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/retessFaces.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lwsserver -legadstatic -L/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -pthread -lm \
-lpthread -lz -lrt -lm
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/vTess /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vTess.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/retessFaces.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lwsserver -legads -lrt
++ for file in `ls *.make`
++ make -f xform.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include xform.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/xform.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/xform /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/xform.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/EGADS/trunk/docs/Tutorial
++ make -f tire.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include tire.c
g++ -g -o tire tire.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ make -f egads2tri.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include egads2tri.c
g++ -g -o egads2tri egads2tri.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lrt -lm
++ cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/EGADS/trunk/docs/EGADS_dot/src
++ make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. circle1_dot.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/circle1_dot.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. pingBodies.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/pingBodies.o
gcc -g -o circle1_dot /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/circle1_dot.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/pingBodies.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lm -lrt
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. circle2_dot.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/circle2_dot.o
gcc -g -o circle2_dot /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/circle2_dot.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/pingBodies.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lm -lrt
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. naca_dot.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/naca_dot.o
gcc -g -o naca_dot /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/naca_dot.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/pingBodies.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lm -lrt
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. ruled_naca_dot.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/ruled_naca_dot.o
gcc -g -o ruled_naca_dot /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/ruled_naca_dot.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/pingBodies.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lm -lrt
++ cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/OpenCSM/trunk/src
++ make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. serveCSM.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/serveCSM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. OpenCSM.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/OpenCSM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udp.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udp.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. tim.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/tim.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libocsm.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libocsm.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libocsm.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/OpenCSM.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udp.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/tim.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lwsserver -ldl -lrt -lm
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/bin/serveCSM /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/serveCSM.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. serveESP.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/serveESP.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/bin/serveESP /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/serveESP.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. sensCSM.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/sensCSM.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/bin/sensCSM /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/sensCSM.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lrt -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpBezier.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpBezier.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/bezier.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/bezier.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/bezier.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpBezier.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpBiconvex.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpBiconvex.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/biconvex.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/biconvex.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/biconvex.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpBiconvex.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpBox.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpBox.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/box.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/box.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/box.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpBox.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpBspline.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpBspline.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/bspline.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/bspline.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/bspline.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpBspline.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfCatmull.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfCatmull.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/catmull.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/catmull.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/catmull.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfCatmull.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfCompare.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfCompare.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/compare.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/compare.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/compare.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfCompare.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfCreateBEM.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfCreateBEM.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/createBEM.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/createBEM.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/createBEM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfCreateBEM.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfCreatePoly.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfCreatePoly.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/createPoly.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/createPoly.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/createPoly.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfCreatePoly.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpCsm.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpCsm.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/csm.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/csm.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/csm.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpCsm.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfDeform.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfDeform.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/deform.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/deform.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/deform.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfDeform.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfDroop.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfDroop.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/droop.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/droop.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/droop.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfDroop.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfDumpPmtrs.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfDumpPmtrs.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/dumpPmtrs.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/dumpPmtrs.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/dumpPmtrs.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfDumpPmtrs.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfEditAttr.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfEditAttr.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/editAttr.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/editAttr.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/editAttr.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfEditAttr.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpEllipse.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpEllipse.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/ellipse.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/ellipse.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/ellipse.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpEllipse.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpEqn2body.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpEqn2body.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/eqn2body.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/eqn2body.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/eqn2body.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpEqn2body.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpFitcurve.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpFitcurve.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/fitcurve.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/fitcurve.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/fitcurve.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpFitcurve.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfFlend.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfFlend.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/flend.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/flend.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/flend.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfFlend.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpFreeform.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpFreeform.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/freeform.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/freeform.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/freeform.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpFreeform.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfGanged.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfGanged.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/ganged.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/ganged.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/ganged.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfGanged.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfGuide.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfGuide.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/guide.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/guide.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/guide.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfGuide.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpHex.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpHex.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/hex.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/hex.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/hex.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpHex.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpImport.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpImport.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/import.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/import.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/import.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpImport.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpKulfan.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpKulfan.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/kulfan.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/kulfan.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/kulfan.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpKulfan.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfLinalg.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfLinalg.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/linalg.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/linalg.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/linalg.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfLinalg.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfMatchBodys.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfMatchBodys.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/matchBodys.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/matchBodys.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/matchBodys.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfMatchBodys.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfMechanism.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfMechanism.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/mechanism.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/mechanism.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/mechanism.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfMechanism.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpNaca.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpNaca.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/naca.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/naca.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/naca.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpNaca.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfNaca6mc.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfNaca6mc.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/naca6mc.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/naca6mc.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/naca6mc.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfNaca6mc.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfNacelle.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfNacelle.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/nacelle.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/nacelle.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/nacelle.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfNacelle.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpNurbbody.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpNurbbody.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/nurbbody.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/nurbbody.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/nurbbody.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpNurbbody.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfNuscale.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfNuscale.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/nuscale.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/nuscale.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/nuscale.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfNuscale.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfOffset.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfOffset.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/offset.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/offset.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/offset.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfOffset.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpParabaloid.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpParabaloid.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/parabaloid.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/parabaloid.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/parabaloid.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpParabaloid.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpParsec.cpp -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpParsec.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/parsec.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/parsec.so
g++ -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/parsec.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpParsec.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpPod.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpPod.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/pod.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/pod.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/pod.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpPod.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpPoly.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpPoly.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/poly.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/poly.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/poly.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpPoly.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfPrintBbox.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfPrintBbox.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/printBbox.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/printBbox.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/printBbox.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfPrintBbox.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfPrintBrep.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfPrintBrep.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/printBrep.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/printBrep.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/printBrep.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfPrintBrep.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfPrintEgo.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfPrintEgo.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/printEgo.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/printEgo.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/printEgo.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfPrintEgo.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpProp.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpProp.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/prop.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/prop.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/prop.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpProp.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpRadwaf.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpRadwaf.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/radwaf.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/radwaf.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/radwaf.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpRadwaf.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpSample.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpSample.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/sample.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/sample.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/sample.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpSample.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpSew.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpSew.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/sew.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/sew.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/sew.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpSew.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfShadow.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfShadow.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/shadow.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/shadow.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/shadow.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfShadow.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfSlices.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfSlices.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/slices.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/slices.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/slices.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfSlices.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpStag.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpStag.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/stag.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/stag.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/stag.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpStag.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfStiffener.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfStiffener.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/stiffener.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/stiffener.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/stiffener.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfStiffener.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpSupell.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpSupell.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/supell.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/supell.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/supell.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpSupell.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfTester1.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfTester1.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/tester1.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/tester1.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/tester1.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfTester1.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpTester2.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpTester2.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/tester2.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/tester2.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/tester2.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpTester2.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpVsp3.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpVsp3.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/vsp3.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/vsp3.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/vsp3.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpVsp3.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpWaffle.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpWaffle.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/waffle.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/waffle.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/waffle.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpWaffle.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udfWarp.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfWarp.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/warp.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/warp.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/warp.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udfWarp.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. eggPDT2.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/eggPDT2.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/PDT2.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/PDT2.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/PDT2.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/eggPDT2.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. udpNaca456.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpNaca456.o
gfortran -g -c -O -fPIC -frecursive -fcray-pointer naca456.f90 -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/naca456.o -J /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/naca456.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/naca456.so
gfortran -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/naca456.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/udpNaca456.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/naca456.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. timEreped.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timEreped.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/ereped.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/ereped.so
g++ -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/ereped.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timEreped.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -lwsserver -legads -ldl -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. timMitten.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timMitten.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/mitten.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/mitten.so
g++ -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/mitten.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timMitten.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. timPlotter.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timPlotter.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/plotter.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/plotter.so
g++ -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/plotter.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timPlotter.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. timPlugs.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timPlugs.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/plugs.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/plugs.so
g++ -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/plugs.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timPlugs.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. timSlugs.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timSlugs.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/slugs.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/slugs.so
g++ -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/slugs.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timSlugs.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -lwsserver -legads -ldl -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. timVspSetup.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timVspSetup.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/vspSetup.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/vspSetup.so
g++ -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/vspSetup.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timVspSetup.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -lwsserver -legads -ldl -lm
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/OpenCSM.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/OpenCSM.h
cp -p OpenCSM.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/OpenCSM.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/common.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/common.h
cp -p common.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/common.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/udp.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/udp.h
cp -p udp.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/udp.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/esp.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/esp.h
cp -p esp.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/esp.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/tim.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/tim.h
cp -p tim.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/tim.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egg.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egg.h
cp -p egg.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/egg.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/udpUtilities.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/udpUtilities.h
cp -p udpUtilities.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/udpUtilities.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/udpUtilities.c
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/udpUtilities.c
cp -p udpUtilities.c /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/udpUtilities.c
++ cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/EGADS/trunk/docs/UDP_UDF/data
++ make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include udpTire.c -o tire.o
gcc -g -o tire tire.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lm -lrt
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DUDP -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include udpTire.c
touch tire.so
rm tire.so
gcc -g -shared -Wl,-no-undefined -o tire.so udpTire.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lm -lrt
++ [[ '' == '' ]]
++ cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS
++ make
(cd src; make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/src'
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/caps.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/caps.h
cp -p ../include/caps.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/caps.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/capsErrors.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/capsErrors.h
cp -p ../include/capsErrors.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/capsErrors.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/capsTypes.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/capsTypes.h
cp -p ../include/capsTypes.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/capsTypes.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aimUtil.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aimUtil.h
cp -p ../include/aimUtil.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aimUtil.h
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aimMesh.h
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aimMesh.h
cp -p ../include/aimMesh.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aimMesh.h
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../include \
-I/usr/include/udunits2 aimUtil.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aimUtil.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include \
-I/usr/include/udunits2 aimTransferUtil.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aimTransferUtil.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../include \
aimMesh.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aimMesh.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libaimUtil.a
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libaimUtil.a
ar -rs /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libaimUtil.a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aimUtil.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aimMesh.o \
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aimTransferUtil.o
ar: creating /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libaimUtil.a
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. \
-I/usr/include/udunits2 capsBase.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/capsBase.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. \
-I/usr/include/udunits2 capsAnalysis.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/capsAnalysis.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. \
-I/usr/include/udunits2 capsApprox.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/capsApprox.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. \
-I/usr/include/udunits2 capsAttr.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/capsAttr.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. \
-I/usr/include/udunits2 capsAIM.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/capsAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. \
-I/usr/include/udunits2 capsBound.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/capsBound.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. \
-I/usr/include/udunits2 capsProblem.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/capsProblem.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. \
-I/usr/include/udunits2 capsValue.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/capsValue.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. \
-I/usr/include/udunits2 capsUnits.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/capsUnits.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. \
-I/usr/include/udunits2 conjGrad.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/conjGrad.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. \
-I/usr/include/udunits2 capsFunIDs.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/capsFunIDs.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. \
-I/usr/include/udunits2 capsChkInpt.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/capsChkInpt.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. \
-I/usr/include/udunits2 printObject.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/printObject.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libcaps.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libcaps.so
(cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj; gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libcaps.so \
capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -ludunits2 -locsm -legads -ldl \
-lrt -lm )
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libcapsstatic.a
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libcapsstatic.a
(cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj; ar -rs /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/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 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libcapsstatic.a
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include testingAIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/testingAIM.o
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/testingAIM.so
rm: cannot remove '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/testingAIM.so': No such file or directory
make[1]: [Makefile:23: /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/testingAIM.so] Error 1 (ignored)
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/testingAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/testingAIM.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include testingWriter.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/testingWriter.o
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/testingWriter.so
rm: cannot remove '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/testingWriter.so': No such file or directory
make[1]: [Makefile:33: /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/testingWriter.so] Error 1 (ignored)
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/testingWriter.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/testingWriter.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -laimUtil -ldl -lrt -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include phaseUtil.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/phaseUtil.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/bin/phaseUtil /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/phaseUtil.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -ludunits2 -locsm -legads -ldl -lrt -lm
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/src'
(cd aim; make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim'
make -C utils
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/utils'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. -DHAVE_PYTHON -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython attrUtils.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/attrUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. -DHAVE_PYTHON -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython meshUtils.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/meshUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. -DHAVE_PYTHON -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cfdUtils.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/cfdUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. -DHAVE_PYTHON -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython miscUtils.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/miscUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. -DHAVE_PYTHON -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython feaUtils.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/feaUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. -DHAVE_PYTHON -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython vlmUtils.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vlmUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. -DHAVE_PYTHON -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranCards.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/nastranCards.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. -DHAVE_PYTHON -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranUtils.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/nastranUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. -DHAVE_PYTHON -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython tecplotUtils.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/tecplotUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. -DHAVE_PYTHON -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython arrayUtils.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/arrayUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. -DHAVE_PYTHON -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython deprecateUtils.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/deprecateUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. -DHAVE_PYTHON -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cardUtils.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/cardUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. -DHAVE_PYTHON -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython jsonUtils.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/jsonUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. -DHAVE_PYTHON -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cython/nastranOP2Reader.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/nastranOP2Reader.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. vlmSpanSpace.cpp -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vlmSpanSpace.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libutils.a
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libutils.a
(cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj; ar -rs /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/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 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libutils.a
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils
cp -p -f arrayUtils.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/arrayUtils.h
cp -p -f attrTypes.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/attrTypes.h
cp -p -f attrUtils.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/attrUtils.h
cp -p -f cardTypes.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/cardTypes.h
cp -p -f cardUtils.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/cardUtils.h
cp -p -f cfdTypes.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/cfdTypes.h
cp -p -f cfdUtils.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/cfdUtils.h
cp -p -f deprecateUtils.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/deprecateUtils.h
cp -p -f feaTypes.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/feaTypes.h
cp -p -f feaUtils.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/feaUtils.h
cp -p -f jsonUtils.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/jsonUtils.h
cp -p -f meshTypes.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/meshTypes.h
cp -p -f meshUtils.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/meshUtils.h
cp -p -f miscTypes.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/miscTypes.h
cp -p -f miscUtils.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/miscUtils.h
cp -p -f nastranCards.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/nastranCards.h
cp -p -f nastranUtils.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/nastranUtils.h
cp -p -f tecplotUtils.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/tecplotUtils.h
cp -p -f vlmSpanSpace.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/vlmSpanSpace.h
cp -p -f vlmTypes.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/vlmTypes.h
cp -p -f vlmUtils.h /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/aim/utils/vlmUtils.h
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/utils'
make -C abaqus
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/abaqus'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils \
abaqusAIM.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/abaqusAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DHAVE_PYTHON -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils \
abaqusUtils.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/abaqusUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils \
-I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/abaqusFILReader.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/abaqusFILReader.o
echo "Building Abaqus with Python"
Building Abaqus with Python
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/abaqusAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/abaqusAIM.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/abaqusUtils.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/abaqusFILReader.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lpthread -ldl -lutil -lm -lm -ldl -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/abaqus'
make -C aflr2
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/aflr2'
gcc -g -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src aflr2_version.c \
-L/home/jenkins/util/AFLR/aflr_lib_11.5.14/Linux-x86-64/lib -laflr2c -lm \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr2_version
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr2_version
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src \
-I../utils aflr2AIM.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr2AIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src \
-I../utils aflr2_Interface.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr2_Interface.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/aflr2AIM.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/aflr2AIM.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/aflr2AIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr2AIM.o \
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr2_Interface.o -L/home/jenkins/util/AFLR/aflr_lib_11.5.14/Linux-x86-64/lib \
-laflr2c -legen -lrec2 -ldftr2 -ldftr3 -ldgeom -lotb -lqtb -lug_io -lug_cpp -lice2 -lug3 -lug2 -lug_gq -lug -lrt -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils \
-laimUtil -locsm -legads -ludunits2 -ldl -lrt -lstdc++ -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/aflr2'
make -C aflr3
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/aflr3'
gcc -g -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src aflr3_version.c \
-L/home/jenkins/util/AFLR/aflr_lib_11.5.14/Linux-x86-64/lib -laflr3 \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr3_version
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr3_version
16.32.50
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src \
aflr3AIM.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr3AIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src \
aflr3_Interface.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr3_Interface.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/EG_getEffBodyTopos.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/EG_getEffBodyTopos.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_check_tess_coord.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_check_tess_coord.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_check_tess_ordering.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_check_tess_ordering.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_get_bedge_coord.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_get_bedge_coord.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_get_edge_spacing.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_get_edge_spacing.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_get_faceOrder.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_get_faceOrder.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_get_face_spacing.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_get_face_spacing.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_get_surf_grid.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_get_surf_grid.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_create_tess.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_create_tess.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_tess_to_dgeom.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_tess_to_dgeom.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_version.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_version.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_auto_cad_geom_setup.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_auto_cad_geom_setup.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_add_attr.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_add_attr.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_add_ff.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_add_ff.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_add_ret_attr.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_add_ret_attr.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_bodyFlag.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_bodyFlag.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_check_bc.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_check_bc.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_data_cleanup.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_data_cleanup.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_edgeData.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_edgeData.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_edgeFace.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_edgeFace.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_edit.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_edit.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_faceEdge.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_faceEdge.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_faceFace.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_faceFace.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_faceFlag.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_faceFlag.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_faceLoop.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_faceLoop.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_file_read.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_file_read.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_file_write.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_file_write.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_idef2idef.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_idef2idef.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_loopEdge.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_loopEdge.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_nodeData.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_nodeData.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_reset_attr.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_reset_attr.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_setup.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_setup.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_write_topo_data.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_write_topo_data.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_curv_at_uv.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_curv_at_uv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_edge_arclen.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_edge_arclen.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_norm_at_uv.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_norm_at_uv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_uv_at_t.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_uv_at_t.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_uv_at_xyz.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_uv_at_xyz.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_uv_bounds.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_uv_bounds.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_xyz_at_u.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_xyz_at_u.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_xyz_at_uv.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_xyz_at_uv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_face_node_map.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_face_node_map.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_faceMatch.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_faceMatch.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_data.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_data.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src /home/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_mzone.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_mzone.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/aflr3AIM.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/aflr3AIM.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/aflr3AIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr3AIM.o \
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr3_Interface.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/EG_getEffBodyTopos.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_check_tess_coord.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_check_tess_ordering.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_get_bedge_coord.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_get_edge_spacing.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_get_faceOrder.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_get_face_spacing.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_get_surf_grid.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_create_tess.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_tess_to_dgeom.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_version.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_auto_cad_geom_setup.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_add_attr.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_add_ff.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_add_ret_attr.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_bodyFlag.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_check_bc.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_data_cleanup.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_edgeData.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_edgeFace.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_edit.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_faceEdge.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_faceFace.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_faceFlag.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_faceLoop.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_file_read.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_file_write.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_idef2idef.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_loopEdge.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_nodeData.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_reset_attr.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_setup.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_write_topo_data.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_curv_at_uv.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_edge_arclen.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_norm_at_uv.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_uv_at_t.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_uv_at_xyz.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_uv_bounds.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_xyz_at_u.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_xyz_at_uv.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_face_node_map.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_faceMatch.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_data.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_mzone.o -L/home/jenkins/util/AFLR/aflr_lib_11.5.14/Linux-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 -lrt -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils \
-laimUtil -locsm -legads -ludunits2 -ldl -lrt -lstdc++ -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/aflr3'
make -C aflr4
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/aflr4'
gcc -g -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src aflr4_version.c \
-L/home/jenkins/util/AFLR/aflr_lib_11.5.14/Linux-x86-64/lib -laflr4 -lm \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr4_version
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr4_version
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src -I../utils aflr4AIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr4AIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/AFLR/aflr_lib_11.5.14/src \
-I../utils aflr4_Interface.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr4_Interface.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/aflr4AIM.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/aflr4AIM.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/aflr4AIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr4AIM.o \
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr4_Interface.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/EG_getEffBodyTopos.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_check_tess_coord.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_check_tess_ordering.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_get_bedge_coord.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_get_edge_spacing.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_get_faceOrder.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_get_face_spacing.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_get_surf_grid.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_create_tess.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_tess_to_dgeom.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_aflr4_version.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_auto_cad_geom_setup.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_add_attr.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_add_ff.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_add_ret_attr.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_bodyFlag.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_check_bc.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_data_cleanup.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_edgeData.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_edgeFace.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_edit.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_faceEdge.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_faceFace.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_faceFlag.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_faceLoop.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_file_read.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_file_write.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_idef2idef.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_loopEdge.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_nodeData.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_reset_attr.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_setup.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_write_topo_data.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_curv_at_uv.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_edge_arclen.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_norm_at_uv.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_uv_at_t.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_uv_at_xyz.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_uv_bounds.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_xyz_at_u.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_eval_xyz_at_uv.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_face_node_map.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_cad_geom_faceMatch.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_data.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads_mzone.o -L/home/jenkins/util/AFLR/aflr_lib_11.5.14/Linux-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 -lrt -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils \
-laimUtil -locsm -legads -ludunits2 -ldl -lrt -lstdc++ -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/aflr4'
make -C astros
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/astros'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils astrosAIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/astrosAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils astrosUtils.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/astrosUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils astrosCards.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/astrosCards.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/astrosAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/astrosAIM.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/astrosUtils.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/astrosCards.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lpthread -ldl -lutil -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/astros'
make -C avl
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/avl'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils avlAIM.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_BODY.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_CNC.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_CPOML.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_DERMATB.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_DERMATM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_DERMATS.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_ELE.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_HINGE.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_STRP.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_SURF.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_TOT.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_VM.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/avlAIM.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/avlAIM.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/avlAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlAIM.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_BODY.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_CNC.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_CPOML.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_DERMATB.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_DERMATM.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_DERMATS.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_ELE.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_HINGE.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_STRP.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_SURF.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_TOT.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlRead_VM.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \
-lstdc++ -lrt -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/avl'
make -C awave
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/awave'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils awaveAIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/awaveAIM.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/awaveAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/awaveAIM.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -std=legacy awavemod.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/awave.o
gfortran -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/awave /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/awave.o
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/awave'
make -C cart3d
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/cart3d'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DCAPS_MESHUTILS -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/libCart3D -I./xddm \
cart3dAIM.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/cart3dAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/c3dio \
-I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/libCart3D -I./xddm \
writeTrix.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/writeTrix.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/c3dio \
-I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/libCart3D \
surfTrix.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/surfTrix.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -pedantic -I./xddm -I. \
`xml2-config --cflags` ./xddm/xddm.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/xddm.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include bodyTess.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/bodyTess.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/cart3dAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/cart3dAIM.o \
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/writeTrix.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/surfTrix.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/xddm.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/bodyTess.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils \
-laimUtil -locsm -legads -ludunits2 -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/ \
-lc3dio -lCart3D -ldl -lxml2 -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include cart3dTest.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/cart3dTest.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/cart3dTest /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/cart3dTest.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -lrt -lm -ldl
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I./xddm \
-I. `xml2-config --cflags` ESPxddm.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/ESPxddm.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/bin/ESPxddm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/ESPxddm.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/writeTrix.o \
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/surfTrix.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/xddm.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/bodyTess.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -locsm -legads \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include/ -lc3dio -lCart3D \
-lpthread -ldl -lxml2 -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/cart3d'
make -C cbaero
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/cbaero'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/cbaeroAIM.o
gcc -g -shared -Wl,-no-undefined /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/cbaeroAIM.o -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/cbaeroAIM.so -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/cbaero'
make -C cgt
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/cgt'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include egads2cgt.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads2cgt.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include aflr4egads.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr4egads.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/egads2cgt /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egads2cgt.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aflr4egads.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads -lcaps -locsm -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/cgt'
make -C custom
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/custom'
make[2]: Nothing to be done for 'default'.
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/custom'
make -C delaundo
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/delaundo'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils delaundoAIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/delaundoAIM.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/delaundoAIM.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/delaundoAIM.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/delaundoAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/delaundoAIM.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/delaundo'
make -C egadsTess
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/egadsTess'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils egadsTessAIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsTessAIM.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/egadsTessAIM.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/egadsTessAIM.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/egadsTessAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/egadsTessAIM.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/egadsTess'
make -C friction
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/friction'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -Wno-format -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils frictionAIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/frictionAIM.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/frictionAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/frictionAIM.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
gfortran -g -c -O -fPIC -frecursive -fcray-pointer friction_eja_mod.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/friction.o
gfortran -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/friction /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/friction.o -static-libgfortran -static-libgcc
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/friction'
make -C fun3d
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/fun3d'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils -I../meshWriter/ugridWriter \
-I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython fun3dAIM.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fun3dAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils -I../meshWriter/ugridWriter \
fun3dUtils.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fun3dUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils \
-I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/fun3dNamelist.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fun3dNamelist.o
Building FUN3D with Python
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/fun3dAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fun3dAIM.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fun3dUtils.o \
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fun3dNamelist.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -ldl -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lpthread -ldl -lutil -lm -lm -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/fun3d'
make -C hsm
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils hsmAIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils hsmUtils.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils hsmAdj.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmAdj.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -Wno-comment rcm/rcm.cpp -DREVISION=7.8 \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/rcm.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 rcm/genrcmi.cpp -DREVISION=7.8 \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/genrcmi.o
make -C src atanc.o
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero atanc.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/atanc.o
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
make -C src bmdump.o
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero bmdump.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/bmdump.o
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
make -C src cross.o
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero cross.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/cross.o
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
make -C src hsmabd.o
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmabd.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmabd.o
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
make -C src hsmbb2.o
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbb2.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmbb2.o
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
make -C src hsmbc.o
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbc.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmbc.o
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
make -C src hsmdep.o
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmdep.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmdep.o
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
make -C src hsmeqn.o
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmeqn.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmeqn.o
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
make -C src hsmgeo.o
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmgeo.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmgeo.o
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
make -C src hsmglr.o
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmglr.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmglr.o
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
make -C src hsmout.o
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmout.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmout.o
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
make -C src hsmprj.o
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmprj.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmprj.o
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
make -C src hsmre1.o
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmre1.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmre1.o
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
make -C src hsmren.o
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmren.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmren.o
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
make -C src hsmrfm.o
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmrfm.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmrfm.o
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
make -C src hsmrun.o
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero -fno-recursive hsmrun.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmrun.o
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
make -C src hsmsol.o
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmsol.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmsol.o
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
make -C src ludcmp.o
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero ludcmp.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/ludcmp.o
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
make -C src sbsolve.o
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero sbsolve.f -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/sbsolve.o
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
make -C src /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libhsm.a
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libhsm.a
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libhsm.a
(cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj; ar -rs /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/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 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libhsm.a
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm/src'
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/hsmAIM.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/hsmAIM.so
gfortran -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/hsmAIM.so \
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmAIM.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmUtils.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmAdj.o \
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/rcm.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/genrcmi.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -lhsm -ldl -lstdc++
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/hsm'
make -C interference
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/interference'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include interferenceAIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/interferenceAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. cloudFns.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/cloudFns.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/interferenceAIM.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/interferenceAIM.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/interferenceAIM.so \
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/interferenceAIM.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/cloudFns.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib \
-laimUtil -locsm -legads -ludunits2 -ldl -lstdc++ -lrt -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/interference'
make -C jfd3
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/jfd3'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils jfd3AIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/jfd3AIM.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/jfd3AIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/jfd3AIM.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/jfd3'
make -C masstran
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/masstran'
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils masstranAIM.cpp \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/masstranAIM.o
g++ -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/masstranAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/masstranAIM.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/masstran'
make -C meshWriter
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter'
make -C bstlWriter
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/bstlWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include bstlWriter.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/bstlWriter.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/bstlWriter.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/bstlWriter.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/bstlWriter'
make -C bvtkWriter
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/bvtkWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include bvtkWriter.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/bvtkWriter.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/bvtkWriter.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/bvtkWriter.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/bvtkWriter'
make -C exodusWriter
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/exodusWriter'
g++ -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/sandialabs/seacas/include -I. exodusWriter.cpp \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/exodusWriter.o
g++ -g -shared -Wl,-no-undefined -std=c++11 -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/exodusWriter.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/exodusWriter.o \
-L/home/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /home/jenkins/util/sandialabs/seacas/lib -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/exodusWriter'
make -C fastWriter
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/fastWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include fastWriter.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fastWriter.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/fastWriter.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fastWriter.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/fastWriter'
make -C libmeshbWriter
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/libmeshbWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include libmeshbWriter.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/libmeshbWriter.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -IlibMeshb/sources -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include libMeshb/sources/libmeshb7.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/libmeshb7.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/libmeshbWriter.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/libmeshbWriter.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/libmeshb7.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/libmeshbWriter'
make -C stlWriter
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/stlWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include stlWriter.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/stlWriter.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/stlWriter.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/stlWriter.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/stlWriter'
make -C su2Writer
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/su2Writer'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include su2Writer.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/su2Writer.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/su2Writer.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/su2Writer.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/su2Writer'
make -C tecplotWriter
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/tecplotWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include tecplotWriter.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/tecplotWriter.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/tecplotWriter.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/tecplotWriter.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/tecplotWriter'
make -C ugridWriter
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/ugridWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include ugridWriter.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/ugridWriter.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/ugridWriter.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/ugridWriter.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/ugridWriter'
make -C vtkWriter
make[3]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/vtkWriter'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include vtkWriter.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vtkWriter.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/vtkWriter.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vtkWriter.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter/vtkWriter'
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/meshWriter'
make -C mses
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/mses'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils msesAIM.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/msesAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils msesUtils.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/msesUtils.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/msesAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/msesAIM.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/msesUtils.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/mses'
make -C mystran
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/mystran'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils mystranAIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/mystranAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils mystranUtils.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/mystranUtils.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/mystranAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/mystranAIM.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/mystranUtils.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lpthread -ldl -lutil -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/mystran'
make -C nastran
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/nastran'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils nastranAIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/nastranAIM.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/nastranAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/nastranAIM.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lpthread -ldl -lutil -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/nastran'
make -C plato
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/plato'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../meshWriter/exodusWriter -I../utils -I/home/jenkins/util/sandialabs/seacas/include -I. platoAIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/platoAIM.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/platoAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/platoAIM.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib \
-L/home/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /home/jenkins/util/sandialabs/seacas/lib \
-laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/plato'
make -C pointwise
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/pointwise'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils pointwiseAIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/pointwiseAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils hashElement.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hashElement.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/pointwiseAIM.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/pointwiseAIM.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/pointwiseAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/pointwiseAIM.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hashElement.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm -lpthread
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/pointwise'
make -C refine
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/refine'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils -I../meshWriter/libmeshbWriter refineAIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/refineAIM.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/refineAIM.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/refineAIM.so
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/refineAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/refineAIM.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/libmeshb7.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/refine'
make -C sierraSD
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/sierraSD'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../meshWriter/exodusWriter -I../utils -I/home/jenkins/util/sandialabs/seacas/include -I. sierraSDAIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/sierraSDAIM.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/sierraSDAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/sierraSDAIM.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib \
-L/home/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /home/jenkins/util/sandialabs/seacas/lib \
-lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/sierraSD'
make -C sierraSM
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/sierraSM'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../meshWriter/exodusWriter -I../utils -I/home/jenkins/util/sandialabs/seacas/include -I. sierraSMAIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/sierraSMAIM.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/sierraSMAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/sierraSMAIM.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib \
-L/home/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /home/jenkins/util/sandialabs/seacas/lib \
-lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/sierraSM'
make -C skeleton
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/skeleton'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils skeletonAIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/skeletonAIM.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/skeletonAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/skeletonAIM.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/skeleton'
make -C spinnaker
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/spinnaker'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include \
-I../meshWriter/exodusWriter \
-I../meshWriter/libmeshbWriter \
-I../utils -I/home/jenkins/util/sandialabs/seacas/include \
-I. \
spinnakerAIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/spinnakerAIM.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/spinnakerAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/spinnakerAIM.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/libmeshb7.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib \
-L/home/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /home/jenkins/util/sandialabs/seacas/lib \
-laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/spinnaker'
make -C su2
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/su2'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../meshWriter/su2Writer -I../utils su2AIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/su2AIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils su2Utils.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/su2Utils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils su2_4_Cardinal.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/su2_4_Cardinal.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils su2_5_Raven.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/su2_5_Raven.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils su2_6_Falcon.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/su2_6_Falcon.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils su2_7_Blackbird.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/su2_7_Blackbird.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils su2_801_Harrier.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/su2_801_Harrier.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/su2AIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/su2AIM.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/su2Utils.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/su2_4_Cardinal.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/su2_5_Raven.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/su2_6_Falcon.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/su2_7_Blackbird.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/su2_801_Harrier.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/su2'
make -C tacs
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/tacs'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils tacsAIM.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/tacsAIM.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/tacsAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/tacsAIM.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lpthread -ldl -lutil -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/tacs'
make -C tetgen
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/tetgen'
g++ -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils tetgenAIM.cpp \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/tetgenAIM.o
g++ -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I/home/jenkins/util/tetgen/tetgen1.6.0 -I../utils \
-DTETLIBRARY tetgen_Interface.cpp -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/tetgen_Interface.o
g++ -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DTETLIBRARY -w /home/jenkins/util/tetgen/tetgen1.6.0/tetgen.cxx -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/tetgen.o
g++ -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -O0 -w /home/jenkins/util/tetgen/tetgen1.6.0/predicates.cxx -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/predicates.o
g++ -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/tetgenAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/tetgenAIM.o \
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/tetgen_Interface.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/tetgen.o \
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/predicates.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -ldl -lrt -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/tetgen'
make -C tsfoil
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/tsfoil'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils \
tsfoilAIM.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/tsfoilAIM.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/tsfoilAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/tsfoilAIM.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/tsfoil'
make -C unitTest
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/unitTest'
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS
cp -p -f pyCAPS/Mesh_Formats.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/Mesh_Formats.py
cp -p -f pyCAPS/test_aflr2.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/test_aflr2.py
cp -p -f pyCAPS/test_aflr3.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/test_aflr3.py
cp -p -f pyCAPS/test_aflr4.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/test_aflr4.py
cp -p -f pyCAPS/test_astros.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/test_astros.py
cp -p -f pyCAPS/test_avl.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/test_avl.py
cp -p -f pyCAPS/test_cart3d.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/test_cart3d.py
cp -p -f pyCAPS/test_cbaero.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/test_cbaero.py
cp -p -f pyCAPS/test_egadsTess.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/test_egadsTess.py
cp -p -f pyCAPS/test_fun3d.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/test_fun3d.py
cp -p -f pyCAPS/test_masstran.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/test_masstran.py
cp -p -f pyCAPS/test_mses.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/test_mses.py
cp -p -f pyCAPS/test_pointwise.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/test_pointwise.py
cp -p -f pyCAPS/test_refine.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/test_refine.py
cp -p -f pyCAPS/test_su2.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/test_su2.py
cp -p -f pyCAPS/test_tacs.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/test_tacs.py
cp -p -f pyCAPS/test_tetgen.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/test_tetgen.py
cp -p -f pyCAPS/test_xfoil.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/test_xfoil.py
cp -p -f pyCAPS/test_zaero.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/test_zaero.py
cp -p -f pyCAPS/Makefile /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/pyCAPS/Makefile
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/csmData
cp -p -f csmData/airfoilSection.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/csmData/airfoilSection.csm
cp -p -f csmData/avlSections.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/csmData/avlSections.csm
cp -p -f csmData/cfd2D.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/csmData/cfd2D.csm
cp -p -f csmData/cfdMultiBody.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/csmData/cfdMultiBody.csm
cp -p -f csmData/cfdSingleBody.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/csmData/cfdSingleBody.csm
cp -p -f csmData/cornerGeom.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/csmData/cornerGeom.csm
cp -p -f csmData/feaSimplePlate.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/csmData/feaSimplePlate.csm
cp -p -f csmData/feaWingBEMAero.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/csmData/feaWingBEMAero.csm
cp -p -f csmData/feaWingOMLAero.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/csmData/feaWingOMLAero.csm
cp -p -f csmData/kulfanSection.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/csmData/kulfanSection.csm
cp -p -f csmData/kulfanSymmetricSection.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/csmData/kulfanSymmetricSection.csm
cp -p -f csmData/masstran.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/csmData/masstran.csm
cp -p -f csmData/multiRegions.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/csmData/multiRegions.csm
cp -p -f csmData/regions.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/csmData/regions.csm
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/aimUnitTest/cCAPS
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/unitTest'
make -C xfoil
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/xfoil'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils \
xfoilAIM.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/xfoilAIM.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/xfoilAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/xfoilAIM.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/xfoil'
make -C zaero
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/zaero'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils zaeroAIM.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/zaeroAIM.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils zaeroUtils.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/zaeroUtils.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils zaeroLinearFlutter.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/zaeroLinearFlutter.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils zaeroTrim.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/zaeroTrim.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils zaeroTypes.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/zaeroTypes.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils zaeroCards.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/zaeroCards.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils zaeroGeneral.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/zaeroGeneral.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../utils zaeroGraphical.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/zaeroGraphical.o
gcc -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/zaeroAIM.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/zaeroAIM.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/zaeroUtils.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/zaeroLinearFlutter.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/zaeroTrim.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/zaeroTypes.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/zaeroCards.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/zaeroGeneral.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/zaeroGraphical.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim/zaero'
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/aim'
(cd Slugs/src; make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/Slugs/src'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. Slugs.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/Slugs.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. Fitter.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/Fitter.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. RedBlackTree.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/RedBlackTree.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. Tessellate.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/Tessellate.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/bin/Slugs /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/Slugs.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/Fitter.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/RedBlackTree.o \
/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/Tessellate.o -lrt -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lwsserver -legads \
-lpthread -lz -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. TestFit.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/TestFit.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/bin/TestFit /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/TestFit.o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/Fitter.o -lrt -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -legads \
-lpthread -lz -lm
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/Slugs/src'
(cd test; make -f aim.make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/test'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include aim.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aim.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/aim /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aim.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads \
-lwsserver -lrt
cp -p -f testingAIM.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/testingAIM.csm
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/test'
(cd test; make -f autoExec.make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/test'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include autoExec.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/autoExec.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/autoExec /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/autoExec.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm \
-legads -lwsserver -lpthread -lrt -lz -lm -ldl
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/test'
(cd test; make -f newPhase.make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/test'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include newPhase.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/newPhase.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/newPhase /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/newPhase.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib \
-lcaps -locsm -legads -lrt -lm -ldl
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/test'
(cd test; make -f basic.make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/test'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include basic.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/basic.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/basic /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/basic.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads\
-lrt -lm -ldl
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/test'
(cd test; make -f geomIn.make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/test'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include geomIn.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/geomIn.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/geomIn /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/geomIn.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads\
-lrt -lm -ldl
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/test'
(cd test; make -f utilsTest.make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/test'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include aimTransferUtilTest.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aimTransferUtilTest.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/aimTransferUtilTest /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aimTransferUtilTest.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -laimUtil -locsm -legads \
-lpthread -lrt -ludunits2 -lm -ldl
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../aim/utils miscUtilsTest.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/miscUtilsTest.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/miscUtilsTest /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/miscUtilsTest.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -laimUtil -locsm -legads \
-lpthread -lrt -ludunits2 -lm -ldl
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I../aim/utils vlmUtilsTest.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vlmUtilsTest.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/vlmUtilsTest /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vlmUtilsTest.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lutils -laimUtil -locsm -legads \
-lpthread -lrt -ludunits2 -lm -ldl
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/test'
(cd test; make -f vVS.make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/test'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include vVS.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vVS.o
g++ -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/vVS /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/vVS.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lwsserver -lrt
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/test'
(cd examples; make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples'
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/analysisData
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite
cp -p -f pyCAPS/abaqus_AGARD445_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/abaqus_AGARD445_PyTest.py
cp -p -f pyCAPS/abaqus_SingleLoadCase_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/abaqus_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/aeroelastic_Iterative_Fun3D_and_Mystran.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aeroelastic_Iterative_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelastic_Iterative_SU2_and_Astros.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aeroelastic_Iterative_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelastic_Iterative_SU2_and_Mystran.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aeroelastic_Iterative_SU2_and_Mystran.py
cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Astros.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Astros.py
cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Mystran.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Nastran.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Nastran.py
cp -p -f pyCAPS/aeroelasticSimple_Displacement_Fun3D_and_Mystran.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aeroelasticSimple_Displacement_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Displacement_SU2_and_Astros.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aeroelasticSimple_Displacement_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelasticSimple_Displacement_SU2_and_Mystran.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aeroelasticSimple_Displacement_SU2_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_Cart3D_and_Mystran.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aeroelasticSimple_Iterative_Cart3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_Fun3D_and_Mystran.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aeroelasticSimple_Iterative_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_SU2_and_Astros.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aeroelasticSimple_Iterative_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_SU2_and_Mystran.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aeroelasticSimple_Iterative_SU2_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Pressure_Fun3D_and_Mystran.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aeroelasticSimple_Pressure_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Pressure_SU2_and_Astros.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aeroelasticSimple_Pressure_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelasticSimple_Pressure_SU2_and_Mystran.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aeroelasticSimple_Pressure_SU2_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Temperature_SU2_and_TACS.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aeroelasticSimple_Temperature_SU2_and_TACS.py
cp -p -f pyCAPS/aflr2_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aflr2_PyTest.py
cp -p -f pyCAPS/aflr4_and_aflr3_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aflr4_and_aflr3_PyTest.py
cp -p -f pyCAPS/aflr4_and_aflr3_Symmetry_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aflr4_and_aflr3_Symmetry_PyTest.py
cp -p -f pyCAPS/aflr4_and_Tetgen_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aflr4_and_Tetgen_PyTest.py
cp -p -f pyCAPS/aflr4_Generic_Missile.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aflr4_Generic_Missile.py
cp -p -f pyCAPS/aflr4_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aflr4_PyTest.py
cp -p -f pyCAPS/aflr4_QuadMesh_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aflr4_QuadMesh_PyTest.py
cp -p -f pyCAPS/aflr4_Symmetry_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aflr4_Symmetry_PyTest.py
cp -p -f pyCAPS/aflr4_tetgen_Regions_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aflr4_tetgen_Regions_PyTest.py
cp -p -f pyCAPS/aflr4_TipTreat_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/aflr4_TipTreat_PyTest.py
cp -p -f pyCAPS/astros_Aeroelastic_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/astros_Aeroelastic_PyTest.py
cp -p -f pyCAPS/astros_AGARD445_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/astros_AGARD445_PyTest.py
cp -p -f pyCAPS/astros_Composite_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/astros_Composite_PyTest.py
cp -p -f pyCAPS/astros_CompositeWingFreq_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/astros_CompositeWingFreq_PyTest.py
cp -p -f pyCAPS/astros_Flutter_15degree.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/astros_Flutter_15degree.py
cp -p -f pyCAPS/astros_MultipleLoadCase_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/astros_MultipleLoadCase_PyTest.py
cp -p -f pyCAPS/astros_OptControl_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/astros_OptControl_PyTest.py
cp -p -f pyCAPS/astros_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/astros_PyTest.py
cp -p -f pyCAPS/astros_SingleLoadCase_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/astros_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/astros_ThreeBarFreq_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/astros_ThreeBarFreq_PyTest.py
cp -p -f pyCAPS/astros_ThreeBarLinkDesign_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/astros_ThreeBarLinkDesign_PyTest.py
cp -p -f pyCAPS/astros_ThreeBarMultiLoad_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/astros_ThreeBarMultiLoad_PyTest.py
cp -p -f pyCAPS/astros_ThreeBar_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/astros_ThreeBar_PyTest.py
cp -p -f pyCAPS/astros_Trim_15degree.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/astros_Trim_15degree.py
cp -p -f pyCAPS/autoLink_Pytest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/autoLink_Pytest.py
cp -p -f pyCAPS/avl_AutoSpan_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/avl_AutoSpan_PyTest.py
cp -p -f pyCAPS/avl_ControlSurf_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/avl_ControlSurf_PyTest.py
cp -p -f pyCAPS/avl_DesignSweep_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/avl_DesignSweep_PyTest.py
cp -p -f pyCAPS/avl_EigenValue_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/avl_EigenValue_PyTest.py
cp -p -f pyCAPS/avl_OpenMDAO_3_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/avl_OpenMDAO_3_PyTest.py
cp -p -f pyCAPS/avl_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/avl_PyTest.py
cp -p -f pyCAPS/awave_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/awave_PyTest.py
cp -p -f pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py
cp -p -f pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py
cp -p -f pyCAPS/cart3d_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/cart3d_PyTest.py
cp -p -f pyCAPS/cbaero_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/cbaero_PyTest.py
cp -p -f pyCAPS/delaundo_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/delaundo_PyTest.py
cp -p -f pyCAPS/egadsTess_Box_Quad_Pytest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/egadsTess_Box_Quad_Pytest.py
cp -p -f pyCAPS/egadsTess_Nose_Quad_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/egadsTess_Nose_Quad_PyTest.py
cp -p -f pyCAPS/egadsTess_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/egadsTess_PyTest.py
cp -p -f pyCAPS/egadsTess_Spheres_Quad_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/egadsTess_Spheres_Quad_PyTest.py
cp -p -f pyCAPS/friction_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/friction_PyTest.py
cp -p -f pyCAPS/fun3d_and_AFLR2_NodeDist_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/fun3d_and_AFLR2_NodeDist_PyTest.py
cp -p -f pyCAPS/fun3d_and_AFLR2_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/fun3d_and_AFLR2_PyTest.py
cp -p -f pyCAPS/fun3d_and_AFLR4_AFLR3_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/fun3d_and_AFLR4_AFLR3_PyTest.py
cp -p -f pyCAPS/fun3d_and_Delaundo_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/fun3d_and_Delaundo_PyTest.py
cp -p -f pyCAPS/fun3d_and_Tetgen_AlphaSweep_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/fun3d_and_Tetgen_AlphaSweep_PyTest.py
cp -p -f pyCAPS/fun3d_and_Tetgen_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/fun3d_and_Tetgen_PyTest.py
cp -p -f pyCAPS/fun3d_Morph_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/fun3d_Morph_PyTest.py
cp -p -f pyCAPS/fun3d_OpenMDAO_3_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/fun3d_OpenMDAO_3_PyTest.py
cp -p -f pyCAPS/fun3d_refine_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/fun3d_refine_PyTest.py
cp -p -f pyCAPS/hsm_CantileverPlate_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/hsm_CantileverPlate_PyTest.py
cp -p -f pyCAPS/hsm_SingleLoadCase_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/hsm_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/masstran_AGARD445_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/masstran_AGARD445_PyTest.py
cp -p -f pyCAPS/masstran_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/masstran_PyTest.py
cp -p -f pyCAPS/mses_OpenMDAO_3_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/mses_OpenMDAO_3_PyTest.py
cp -p -f pyCAPS/mses_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/mses_PyTest.py
cp -p -f pyCAPS/mystran_AGARD445_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/mystran_AGARD445_PyTest.py
cp -p -f pyCAPS/mystran_MultiLoadCase_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/mystran_MultiLoadCase_PyTest.py
cp -p -f pyCAPS/mystran_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/mystran_PyTest.py
cp -p -f pyCAPS/mystran_SingleLoadCase_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/mystran_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/nastran_Aeroelastic_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/nastran_Aeroelastic_PyTest.py
cp -p -f pyCAPS/nastran_AGARD445_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/nastran_AGARD445_PyTest.py
cp -p -f pyCAPS/nastran_Composite_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/nastran_Composite_PyTest.py
cp -p -f pyCAPS/nastran_CompositeWingDesign_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/nastran_CompositeWingDesign_PyTest.py
cp -p -f pyCAPS/nastran_CompositeWingFreq_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/nastran_CompositeWingFreq_PyTest.py
cp -p -f pyCAPS/nastran_Flutter_15degree.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/nastran_Flutter_15degree.py
cp -p -f pyCAPS/nastran_MultiLoadCase_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/nastran_MultiLoadCase_PyTest.py
cp -p -f pyCAPS/nastran_OptimizationMultiLoad_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/nastran_OptimizationMultiLoad_PyTest.py
cp -p -f pyCAPS/nastran_PlateMisc_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/nastran_PlateMisc_PyTest.py
cp -p -f pyCAPS/nastran_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/nastran_PyTest.py
cp -p -f pyCAPS/nastran_SingleLoadCase_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/nastran_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarDesign_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/nastran_ThreeBarDesign_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarFreq_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/nastran_ThreeBarFreq_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarLinkDesign_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/nastran_ThreeBarLinkDesign_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarMultiLoad_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/nastran_ThreeBarMultiLoad_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBar_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/nastran_ThreeBar_PyTest.py
cp -p -f pyCAPS/nastran_Trim_15degree.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/nastran_Trim_15degree.py
cp -p -f pyCAPS/plato_aflr_airfoil_morph_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/plato_aflr_airfoil_morph_PyTest.py
cp -p -f pyCAPS/plato_aflr_airfoil_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/plato_aflr_airfoil_PyTest.py
cp -p -f pyCAPS/plato_aflr_cyli_box_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/plato_aflr_cyli_box_PyTest.py
cp -p -f pyCAPS/plato_aflr_table_morph_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/plato_aflr_table_morph_PyTest.py
cp -p -f pyCAPS/plato_aflr_table_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/plato_aflr_table_PyTest.py
cp -p -f pyCAPS/plato_aflr_tetgen_cyli_box_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/plato_aflr_tetgen_cyli_box_PyTest.py
cp -p -f pyCAPS/plato_aflr_tetgen_table_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/plato_aflr_tetgen_table_PyTest.py
cp -p -f pyCAPS/plato_tetgen_cyli_box_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/plato_tetgen_cyli_box_PyTest.py
cp -p -f pyCAPS/plato_tetgen_table_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/plato_tetgen_table_PyTest.py
cp -p -f pyCAPS/pointwise_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/pointwise_PyTest.py
cp -p -f pyCAPS/pointwise_Symmetry_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/pointwise_Symmetry_PyTest.py
cp -p -f pyCAPS/su2_and_AFLR2_NodeDist_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/su2_and_AFLR2_NodeDist_PyTest.py
cp -p -f pyCAPS/su2_and_AFLR2_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/su2_and_AFLR2_PyTest.py
cp -p -f pyCAPS/su2_and_AFLR4_AFLR3_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/su2_and_AFLR4_AFLR3_PyTest.py
cp -p -f pyCAPS/su2_and_Delaundo_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/su2_and_Delaundo_PyTest.py
cp -p -f pyCAPS/su2_and_pointwise_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/su2_and_pointwise_PyTest.py
cp -p -f pyCAPS/su2_and_Tetgen_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/su2_and_Tetgen_PyTest.py
cp -p -f pyCAPS/su2_Morph_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/su2_Morph_PyTest.py
cp -p -f pyCAPS/su2_X43a_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/su2_X43a_PyTest.py
cp -p -f pyCAPS/tetgen_Holes_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/tetgen_Holes_PyTest.py
cp -p -f pyCAPS/tetgen_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/tetgen_PyTest.py
cp -p -f pyCAPS/tetgen_Regions_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/tetgen_Regions_PyTest.py
cp -p -f pyCAPS/tsfoil_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/tsfoil_PyTest.py
cp -p -f pyCAPS/xfoil_PyTest.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/pyCAPS/xfoil_PyTest.py
cp -p -f csmData/15degreeWing.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/15degreeWing.csm
cp -p -f csmData/aeroelasticDataTransfer.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/aeroelasticDataTransfer.csm
cp -p -f csmData/aeroelasticDataTransferSimple.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/aeroelasticDataTransferSimple.csm
cp -p -f csmData/airfoilSection.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/airfoilSection.csm
cp -p -f csmData/avlWing.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/avlWing.csm
cp -p -f csmData/avlWings.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/avlWings.csm
cp -p -f csmData/avlWingTail.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/avlWingTail.csm
cp -p -f csmData/awaveWingTailFuselage.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/awaveWingTailFuselage.csm
cp -p -f csmData/cfd2DArbShape.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/cfd2DArbShape.csm
cp -p -f csmData/cfd2D.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/cfd2D.csm
cp -p -f csmData/cfd_airfoilSection.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/cfd_airfoilSection.csm
cp -p -f csmData/cfdMultiBody.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/cfdMultiBody.csm
cp -p -f csmData/cfdSymmetry.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/cfdSymmetry.csm
cp -p -f csmData/cfdX43a.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/cfdX43a.csm
cp -p -f csmData/compositeWing.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/compositeWing.csm
cp -p -f csmData/cyli_box_shell.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/cyli_box_shell.csm
cp -p -f csmData/cyli_box_solid.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/cyli_box_solid.csm
cp -p -f csmData/feaAGARD445.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/feaAGARD445.csm
cp -p -f csmData/feaBoxes.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/feaBoxes.csm
cp -p -f csmData/feaCantileverPlate.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/feaCantileverPlate.csm
cp -p -f csmData/feaJoinedPlate.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/feaJoinedPlate.csm
cp -p -f csmData/feaSimplePlate.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/feaSimplePlate.csm
cp -p -f csmData/feaThreeBar.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/feaThreeBar.csm
cp -p -f csmData/feaWingBEMAero.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/feaWingBEMAero.csm
cp -p -f csmData/feaWingBEM.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/feaWingBEM.csm
cp -p -f csmData/frictionWingTailFuselage.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/frictionWingTailFuselage.csm
cp -p -f csmData/generic_missile.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/generic_missile.csm
cp -p -f csmData/interference.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/interference.csm
cp -p -f csmData/linearAero.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/linearAero.csm
cp -p -f csmData/nosecone1.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/nosecone1.csm
cp -p -f csmData/regions.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/regions.csm
cp -p -f csmData/simpleWingBox.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/simpleWingBox.csm
cp -p -f csmData/spheres.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/spheres.csm
cp -p -f csmData/table.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/table.csm
cp -p -f csmData/tiptreat.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/tiptreat.csm
cp -p -f csmData/avlWing.udc /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/csmData/avlWing.udc
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/analysisData/nastran
cp -p -f analysisData/nastran/NastranAeroWingBEM.f06 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/analysisData/nastran/NastranAeroWingBEM.f06
cp -p -f analysisData/nastran/NastranCompositePlate.f06 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/analysisData/nastran/NastranCompositePlate.f06
cp -p -f analysisData/nastran/NastranCompositeWing_Design.f06 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/analysisData/nastran/NastranCompositeWing_Design.f06
cp -p -f analysisData/nastran/NastranCompositeWing_Freq.f06 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/analysisData/nastran/NastranCompositeWing_Freq.f06
cp -p -f analysisData/nastran/NastranFlutter15Deg.f06 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/analysisData/nastran/NastranFlutter15Deg.f06
cp -p -f analysisData/nastran/NastranMiscLoadPlate.f06 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/analysisData/nastran/NastranMiscLoadPlate.f06
cp -p -f analysisData/nastran/NastranModalAGARD445.f06 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/analysisData/nastran/NastranModalAGARD445.f06
cp -p -f analysisData/nastran/NastranMultiLoadPlate.f06 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/analysisData/nastran/NastranMultiLoadPlate.f06
cp -p -f analysisData/nastran/NastranOptMultiLoadPlate.f06 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/analysisData/nastran/NastranOptMultiLoadPlate.f06
cp -p -f analysisData/nastran/NastranSingleLoadPlate.f06 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/analysisData/nastran/NastranSingleLoadPlate.f06
cp -p -f analysisData/nastran/NastranThreeBarDesign.f06 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/analysisData/nastran/NastranThreeBarDesign.f06
cp -p -f analysisData/nastran/NastranThreeBar.f06 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/analysisData/nastran/NastranThreeBar.f06
cp -p -f analysisData/nastran/NastranThreeBarFreq.f06 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/analysisData/nastran/NastranThreeBarFreq.f06
cp -p -f analysisData/nastran/NastranThreeBarLinkDesign.f06 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/analysisData/nastran/NastranThreeBarLinkDesign.f06
cp -p -f analysisData/nastran/NastranThreeBarMultiLoad.f06 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/analysisData/nastran/NastranThreeBarMultiLoad.f06
cp -p -f analysisData/nastran/NastranTrim15Deg.f06 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/analysisData/nastran/NastranTrim15Deg.f06
cp -p -f analysisData/nastran/NastranWingBEM.f06 /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/analysisData/nastran/NastranWingBEM.f06
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/capsPhase/csm
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/capsPhase/pyCAPS
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/csm
mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/pyCAPS
cp -p -f corsairlite/boydBox.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/boydBox.py
cp -p -f corsairlite/gp.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/gp.py
cp -p -f corsairlite/hoburg_blackbox.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/hoburg_blackbox.py
cp -p -f corsairlite/hoburg_gp.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/hoburg_gp.py
cp -p -f corsairlite/qp.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/qp.py
cp -p -f corsairlite/sp.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/sp.py
cp -p -f corsairlite/capsPhase/csm/wing1.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/capsPhase/csm/wing1.csm
cp -p -f corsairlite/capsPhase/csm/wing2.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/capsPhase/csm/wing2.csm
cp -p -f corsairlite/capsPhase/pyCAPS/optTaperAvl.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/capsPhase/pyCAPS/optTaperAvl.py
cp -p -f corsairlite/capsPhase/pyCAPS/optWingAvl.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/capsPhase/pyCAPS/optWingAvl.py
cp -p -f corsairlite/capsPhase/pyCAPS/sizeWing.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/capsPhase/pyCAPS/sizeWing.py
cp -p -f corsairlite/multifidelity/csm/naca.csm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/csm/naca.csm
cp -p -f corsairlite/multifidelity/pyCAPS/Camber.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/pyCAPS/Camber.py
cp -p -f corsairlite/multifidelity/pyCAPS/CMConstraint.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/pyCAPS/CMConstraint.py
cp -p -f corsairlite/multifidelity/pyCAPS/FlowTrip.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/pyCAPS/FlowTrip.py
cp -p -f corsairlite/multifidelity/pyCAPS/fullModelKulfan.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/pyCAPS/fullModelKulfan.py
cp -p -f corsairlite/multifidelity/pyCAPS/fullModelNACA.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/pyCAPS/fullModelNACA.py
cp -p -f corsairlite/multifidelity/pyCAPS/GPSize.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/pyCAPS/GPSize.py
cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan2.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/pyCAPS/Kulfan2.py
cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan4.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/pyCAPS/Kulfan4.py
cp -p -f corsairlite/multifidelity/pyCAPS/MSES.py /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/pyCAPS/MSES.py
cp -p -f regressionTest/execute_CTestRegression.sh /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/execute_CTestRegression.sh
cp -p -f regressionTest/execute_PyTestRegression.sh /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/execute_PyTestRegression.sh
(make -C cCAPS -f aeroelastic_SU2.make)
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include avlTest.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlTest.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/avlTest /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/avlTest.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -legads -locsm \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include awaveTest.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/awaveTest.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/awaveTest /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/awaveTest.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -legads -locsm \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include frictionTest.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/frictionTest.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/frictionTest /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/frictionTest.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include fun3dAFLR2Test.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fun3dAFLR2Test.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/fun3dAFLR2Test /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fun3dAFLR2Test.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include fun3dTetgenTest.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fun3dTetgenTest.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/fun3dTetgenTest /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/fun3dTetgenTest.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include aeroelasticTest.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aeroelasticTest.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/aeroelasticTest /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/aeroelasticTest.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f hsm.make)
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include hsmTest.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmTest.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/hsmTest /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmTest.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include hsmSimplePlateTest.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmSimplePlateTest.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/hsmSimplePlateTest /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmSimplePlateTest.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include hsmCantileverPlateTest.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmCantileverPlateTest.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/hsmCantileverPlateTest /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmCantileverPlateTest.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include hsmJoinedPlateTest.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmJoinedPlateTest.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/hsmJoinedPlateTest /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/hsmJoinedPlateTest.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include interferenceTest.c \
-o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/interferenceTest.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/interferenceTest /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/interferenceTest.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include msesTest.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/msesTest.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/msesTest /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/msesTest.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -legads -locsm \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f mystran.make)
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include mystranTest.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/mystranTest.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/mystranTest /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/mystranTest.o \
-L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include pointwiseTest.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/pointwiseTest.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/pointwiseTest /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/pointwiseTest.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples'
+++ find /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/training/ -name Makefile
++ for i in `find $WORKSPACE/CAPS/training/ -name Makefile`
++ [[ /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/training/2023/lectures/Makefile == *\l\e\c\t\u\r\e\s* ]]
++ continue
++ for i in `find $WORKSPACE/CAPS/training/ -name Makefile`
++ [[ /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/training/2023/data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]]
+++ dirname /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/training/2023/data/session01/Makefile
++ cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/training/2023/data/session01
++ make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include template_avl.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/template_avl.o
gcc -g -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/template_avl /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/template_avl.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -legads -lrt -lm -ldl
++ for i in `find $WORKSPACE/CAPS/training/ -name Makefile`
++ [[ /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/training/data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]]
+++ dirname /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/training/data/session01/Makefile
++ cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/training/data/session01
++ make
make: Nothing to be done for 'default'.
++ cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/OpenCSM/trunk/src
++ make -f serveESP.make
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. timCapsMode.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timCapsMode.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/capsMode.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/capsMode.so
g++ -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/capsMode.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timCapsMode.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. timFlowchart.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timFlowchart.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/flowchart.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/flowchart.so
g++ -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/flowchart.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timFlowchart.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. timViewer.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timViewer.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/viewer.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/viewer.so
g++ -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/viewer.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timViewer.o -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/include -I. -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 timPyscript.c -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timPyscript.o
touch /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/pyscript.so
rm /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/pyscript.so
g++ -g -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib/pyscript.so /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/obj/timPyscript.o -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lpthread -ldl -lutil -lm -L/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/lib -lcaps -locsm -lwsserver -legads -ldl -lrt -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
++ ln -f -s /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/OpenCSM/trunk/udc /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64
+++ find /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/OpenCSM/trunk/data/training/ -name Makefile
+ mkdir -p /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/test
+ cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/test
+ source /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/JenkinsESP/RunRegression.sh
++ [[ 0 == 1 ]]
++ [[ 0 == 2 ]]
++ [[ /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64 == '' ]]
++ [[ CAPS/LINEARAERO == '' ]]
++ [[ 7.8 == '' ]]
++ [[ ! -d /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/JenkinsESP ]]
++ rm -f csmFiles.txt
++ [[ CAPS/LINEARAERO =~ [0-9]+.[0-9]+ ]]
++ export ESPTEST=CAPS/LINEARAERO
++ ESPTEST=CAPS/LINEARAERO
++ [[ CAPS/LINEARAERO == \C\A\P\S* ]]
++ [[ ! -d /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS ]]
++ export CAPSTARGET=LINEARAERO
++ CAPSTARGET=LINEARAERO
++ [[ LINEARAERO == \u\n\i\t ]]
++ [[ LINEARAERO == \t\r\a\i\n\i\n\g\2\0\1\8 ]]
++ [[ LINEARAERO == \t\r\a\i\n\i\n\g ]]
++ [[ LINEARAERO == *\_\o\f\f ]]
++ cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/
++ make test TYPE=LINEARAERO
(make -C cCAPS -f aeroelastic_SU2.make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
make[1]: '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
make[1]: '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/avlTest' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
make[1]: '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/awaveTest' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
make[1]: '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/frictionTest' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
make[1]: Nothing to be done for 'fun3d'.
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f hsm.make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
make[1]: 'hsm' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
make[1]: '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/interferenceTest' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
make[1]: '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/msesTest' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f mystran.make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
make[1]: '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/mystranTest' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[1]: Entering directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
make[1]: '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/cCAPS/pointwiseTest' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/examples/cCAPS'
(cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest; ./execute_CTestRegression.sh LINEARAERO)
Running.... LINEARAERO c-Tests
=================================================
+ echo './avlTest test;'
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/cCAPSlog.txt
./avlTest test;
+ ./avlTest 0
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/cCAPSlog.txt
Attention: avlTest is hard coded to look for ../csmData/avlWingTail.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice control surface data
VLM control surface name - WingRightLE
VLM control surface name - WingRightTE
VLM control surface name - Tail
Done getting vortex lattice control surface data
Getting vortex lattice surface data
VLM surface name - Wing
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Writing surface - Vertical_Tail (ID = 1)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Running AVL!
Value of Cltot = 0.619913
StripForces
Wing = {"Xle":[1.565221892029e+00,1.512117367810e+00,1.409527304938e+00,1.264443046659e+00,1.086751845411e+00,8.885630629098e-01,6.833829371601e-01,4.851941546545e-01,3.075029533974e-01,1.624186951053e-01,5.982863221714e-02,6.724107980270e-03,6.724107971058e-03,5.982863219013e-02,1.624186950623e-01,3.075029533414e-01,4.851941545893e-01,6.833829370902e-01,8.885630628399e-01,1.086751845346e+00,1.264443046603e+00,1.409527304895e+00,1.512117367783e+00,1.565221892020e+00],"Yle":[-3.856416046770e+00,-3.725576361740e+00,-3.472813499993e+00,-3.115352832843e+00,-2.677554714026e+00,-2.189254361841e+00,-1.683728638332e+00,-1.195428286135e+00,-7.576301672945e-01,-4.001695001132e-01,-1.474066383261e-01,-1.656695325269e-02,1.656695322999e-02,1.474066382596e-01,4.001695000074e-01,7.576301671565e-01,1.195428285974e+00,1.683728638159e+00,2.189254361668e+00,2.677554713865e+00,3.115352832706e+00,3.472813499887e+00,3.725576361674e+00,3.856416046747e+00],"Zle":[2.486597711706e-01,2.402232939480e-01,2.239252714835e-01,2.008763870743e-01,1.726473841027e-01,1.411620224705e-01,1.085659775407e-01,7.708061590764e-02,4.885161293456e-02,2.580272852328e-02,9.504706056265e-03,1.068228830823e-03,1.068228829360e-03,9.504706051974e-03,2.580272851645e-02,4.885161292566e-02,7.708061589728e-02,1.085659775295e-01,1.411620224593e-01,1.726473840924e-01,2.008763870654e-01,2.239252714767e-01,2.402232939437e-01,2.486597711692e-01],"Chord":[9.710071581587e-01,9.928137666999e-01,1.034940899447e+00,1.094517661923e+00,1.167483996219e+00,1.248867367237e+00,1.333121632734e+00,1.414505003754e+00,1.487471338054e+00,1.547048100535e+00,1.589175233289e+00,1.610981841837e+00,1.610981841841e+00,1.589175233300e+00,1.547048100553e+00,1.487471338077e+00,1.414505003781e+00,1.333121632763e+00,1.248867367266e+00,1.167483996246e+00,1.094517661946e+00,1.034940899465e+00,9.928137667110e-01,9.710071581625e-01],"Area":[6.420432739224e-02,1.924649501823e-01,3.191588402418e-01,4.398794051499e-01,5.463997379092e-01,6.272332670617e-01,6.695492724342e-01,6.620092145623e-01,5.978048871833e-01,4.770843222898e-01,3.080744268775e-01,1.065203328294e-01,1.065203327570e-01,3.080744268129e-01,4.770843222394e-01,5.978048871514e-01,6.620092145502e-01,6.695492724407e-01,6.272332670835e-01,5.463997379421e-01,4.398794051895e-01,3.191588402846e-01,1.924649502262e-01,6.420432743628e-02],"c_cl":[1.751976980131e-01,4.816388142980e-01,7.134545983425e-01,8.955798774854e-01,1.045275116632e+00,1.165642609066e+00,1.251488483106e+00,1.294909342036e+00,1.290147495293e+00,1.237589733955e+00,1.147354354590e+00,1.069716379938e+00,1.027204841580e+00,9.123069911140e-01,8.271224835189e-01,7.465072383829e-01,6.622506856527e-01,5.718077594720e-01,4.773770050905e-01,3.839108464455e-01,2.965810831881e-01,2.166269422082e-01,1.372747954618e-01,4.847522879861e-02],"ai":[2.423376448062e-01,1.891573605670e-01,1.387726073610e-01,1.136377561111e-01,1.056109957988e-01,1.077519869781e-01,1.163918473304e-01,1.297918603655e-01,1.465983278745e-01,1.624995174599e-01,1.707158095744e-01,1.656351191924e-01,-7.833998870069e-02,-4.190817556549e-02,-1.699095118251e-02,-7.589503463209e-04,7.958849673328e-03,1.019416065192e-02,8.688915578666e-03,6.053380335367e-03,5.120395027035e-03,9.296755297874e-03,2.004804046071e-02,3.330492577589e-02],"cl_norm":[2.044051829732e-01,5.494672225944e-01,7.808579037671e-01,9.268407130709e-01,1.014078158136e+00,1.057019341176e+00,1.062951411332e+00,1.036333388588e+00,9.816462634657e-01,9.051794884122e-01,8.167547094735e-01,7.499676468301e-01,7.211772113982e-01,6.503467495440e-01,6.057660560789e-01,5.686988847409e-01,5.305932247986e-01,4.861412346272e-01,4.332732553839e-01,3.727603475171e-01,3.071901673660e-01,2.373206031159e-01,1.568074209169e-01,5.666485024198e-02],"cl":[1.803741931756e-01,4.848688546459e-01,6.890559834545e-01,8.178762563197e-01,8.948575908405e-01,9.327503738523e-01,9.379850374388e-01,9.144963748400e-01,8.662385668552e-01,7.987616435483e-01,7.207325646090e-01,6.617973538495e-01,6.363916792641e-01,5.738884333905e-01,5.345488897546e-01,5.018395375447e-01,4.682137871232e-01,4.289878157188e-01,3.823352848870e-01,3.289366049983e-01,2.710752133784e-01,2.094198967381e-01,1.383722840117e-01,5.000302093687e-02],"cd":[4.708816796028e-03,1.893013552462e-02,2.388458719217e-02,2.809788812561e-02,3.450496926232e-02,4.310977683936e-02,5.296690620751e-02,6.273588035908e-02,7.092746653695e-02,7.623132904850e-02,7.793919402374e-02,1.330641046361e-01,7.642533954139e-02,1.575280561794e-02,1.020926164300e-02,5.734996040044e-03,2.453990236882e-03,7.034156944428e-05,-1.681061755696e-03,-2.904871637687e-03,-3.696799546922e-03,-4.291551637882e-03,-4.755989795807e-03,-4.178738547375e-03],"cdv":[0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00],"cm_c/4":[-6.175122770635e-02,-1.541367450249e-01,-1.990020049078e-01,-2.179523703798e-01,-2.259241556000e-01,-2.291785023832e-01,-2.301045091168e-01,-2.293937884749e-01,-2.266765134794e-01,-2.205756980543e-01,-2.089282623641e-01,-1.947906406100e-01,-1.847119741766e-01,-1.559354818193e-01,-1.355315131375e-01,-1.232795365876e-01,-1.170486694971e-01,-1.141869860843e-01,-1.128288355904e-01,-1.117855412669e-01,-1.094863434133e-01,-1.016126232940e-01,-7.889656776610e-02,-3.215621313960e-02],"cm_LE":[-9.907391078332e-02,-2.553625521061e-01,-3.443180862961e-01,-3.917771248736e-01,-4.170475207536e-01,-4.288879437379e-01,-4.309998082915e-01,-4.249313258859e-01,-4.112512348868e-01,-3.899661415023e-01,-3.610798550199e-01,-3.345295675168e-01,-3.190696575594e-01,-2.776668920570e-01,-2.496150543394e-01,-2.306580335187e-01,-2.170714278267e-01,-2.053105443164e-01,-1.932221818518e-01,-1.798625218874e-01,-1.643057066258e-01,-1.427050164900e-01,-1.051753523064e-01,-4.137433282282e-02],"C.P.x/c":[5.923506801011e-01,5.678936810397e-01,5.388038268097e-01,5.164857534324e-01,5.024693961503e-01,4.957018606561e-01,4.953178888067e-01,5.008416597223e-01,5.116790825907e-01,5.261470832205e-01,5.398832002650e-01,5.443357803971e-01,5.402488831882e-01,5.217174153487e-01,5.035437183300e-01,4.956552889212e-01,4.999897967897e-01,5.161776906017e-01,5.451044281036e-01,5.898391652626e-01,6.538965497758e-01,7.352099770687e-01,8.201760893057e-01,8.930854083837e-01]}
Vertical_Tail = {"Xle":[5.481142821257e+00,5.457739875756e+00,5.413224828118e+00,5.351955121359e+00,5.279928261269e+00,5.204194738752e+00,5.132167878660e+00,5.070898171897e+00,5.026383124254e+00,5.002980178746e+00],"Yle":[0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00],"Zle":[1.462285642514e+00,1.415479751513e+00,1.326449656236e+00,1.203910242719e+00,1.059856522538e+00,9.083894775049e-01,7.643357573198e-01,6.417963437947e-01,5.527662485071e-01,5.059603574925e-01],"Chord":[7.291641787429e-01,7.525671242437e-01,7.970821718820e-01,8.583518786405e-01,9.303787387310e-01,1.006112261248e+00,1.078139121340e+00,1.139408828103e+00,1.183923875746e+00,1.207326821254e+00],"Area":[1.727730179136e-02,5.174997687051e-02,8.537019049526e-02,1.158415604078e-01,1.391867381176e-01,1.505166423044e-01,1.455036346588e-01,1.220345306258e-01,8.141205112924e-02,2.860720599220e-02],"c_cl":[4.143502484414e-02,1.146121890396e-01,1.669674480703e-01,2.000258625573e-01,2.165069436646e-01,2.173612378312e-01,2.020982864237e-01,1.687203348323e-01,1.143884794128e-01,4.073751989354e-02],"ai":[2.065296924522e-01,1.849180223914e-01,1.591285664756e-01,1.456224964407e-01,1.435231644005e-01,1.506386553618e-01,1.666466052404e-01,1.914179167691e-01,2.193221173425e-01,2.365321328628e-01],"cl_norm":[6.579957348169e-02,1.763463053599e-01,2.425545992659e-01,2.698370559981e-01,2.694590983034e-01,2.501591871284e-01,2.170544160377e-01,1.714623014101e-01,1.118766125248e-01,3.907064104101e-02],"cl":[5.682537081783e-02,1.522949719000e-01,2.094733190131e-01,2.330348048799e-01,2.327083956797e-01,2.160407403859e-01,1.874510278159e-01,1.480770823176e-01,9.661810337313e-02,3.374191575669e-02],"cd":[4.670566079253e-03,1.374698956981e-02,1.845844898547e-02,2.032218684719e-02,2.072187092666e-02,2.023884851592e-02,1.896705322926e-02,1.657142171115e-02,1.222733795463e-02,5.106244760902e-03],"cdv":[0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00],"cm_c/4":[-3.303465544541e-02,-8.761746958831e-02,-1.194746602280e-01,-1.341488123561e-01,-1.380350789960e-01,-1.339349413678e-01,-1.218867053322e-01,-1.002593790934e-01,-6.716156843016e-02,-2.373448304331e-02],"cm_LE":[-4.232877133353e-02,-1.126299441675e-01,-1.539951982648e-01,-1.724118490114e-01,-1.757829360721e-01,-1.683239687781e-01,-1.510824211714e-01,-1.228726806386e-01,-8.171902803712e-02,-2.878672165370e-02],"C.P.x/c":[8.313363814434e-01,8.253142634664e-01,8.203574125380e-01,8.256599853196e-01,8.431675932571e-01,8.699522420104e-01,9.002322593395e-01,9.270755982237e-01,9.451240614898e-01,9.534124326094e-01]}
real 0m0.409s
user 0m0.335s
sys 0m0.065s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./avlTest passed (as expected)
=============================================
=================================================
+ echo './msesTest test;'
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/cCAPSlog.txt
./msesTest test;
+ ./msesTest 0
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/cCAPSlog.txt
Attention: msesTest is hard coded to look for ../csmData/airfoilSection.csm
Value of CL = 0.276892
real 0m3.103s
user 0m3.012s
sys 0m0.082s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./msesTest passed (as expected)
=============================================
=================================================
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/cCAPSlog.txt
+ echo './awaveTest test;'
./awaveTest test;
+ ./awaveTest 0
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/cCAPSlog.txt
Attention: awaveTest is hard coded to look for ../csmData/awaveWingTailFuselage.csm
Writing Awave input file
Body Section, Body ID 1
XCG: 1.571025 -3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :RightWingTank
Awave TYPE: 3
Body Section, Body ID 2
XCG: 2.539271 -3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :RightWingTank
Awave TYPE: 3
Body Section, Body ID 3
XCG: 1.571025 3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :LeftWingTank
Awave TYPE: 3
Body Section, Body ID 4
XCG: 2.539271 3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :LeftWingTank
Awave TYPE: 3
Lifting Surface Section, Body ID 5
XLE: 1.571946 -3.872983 0.249728
CHORD: 0.968408
ATTRIB:Wing
NAME :Wing
Awave TYPE: 0
Lifting Surface Section, Body ID 6
XLE: 0.000000 0.000000 0.000000
CHORD: 1.614013
ATTRIB:Wing
NAME :Wing
Awave TYPE: 1
Lifting Surface Section, Body ID 7
XLE: 1.571946 3.872983 0.249728
CHORD: 0.968408
ATTRIB:Wing
NAME :Wing
Awave TYPE: 1
Lifting Surface Section, Body ID 8
XLE: 5.484123 0.000000 1.468246
CHORD: 0.726185
ATTRIB:VTail
NAME :VertTail
Awave TYPE: 4
Lifting Surface Section, Body ID 9
XLE: 5.000000 0.000000 0.500000
CHORD: 1.210308
ATTRIB:VTail
NAME :VertTail
Awave TYPE: 4
Lifting Surface Section, Body ID 10
XLE: 5.484123 -0.968246 0.500000
CHORD: 0.726185
ATTRIB:HTail
NAME :Stab
Awave TYPE: 0
Lifting Surface Section, Body ID 11
XLE: 5.484123 0.000000 0.500000
CHORD: 0.726185
ATTRIB:HTail
NAME :Stab
Awave TYPE: 5
Lifting Surface Section, Body ID 12
XLE: 5.484123 0.968246 0.500000
CHORD: 0.726185
ATTRIB:HTail
NAME :Stab
Awave TYPE: 5
Body Section, Body ID 13
XCG: -2.000000 0.000000 0.000000
AREA: 0.000000
RAD: 0.000000
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
Body Section, Body ID 14
XCG: 0.000000 -0.000000 -0.000000
AREA: 0.818123
RAD: 0.510310
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
Warning: capsGroup not found on body 15!
Body Section, Body ID 15
XCG: 1.613743 -0.000000 0.000000
AREA: 0.327249
RAD: 0.322749
ATTRIB:Fuse
NAME :(null)
Awave TYPE: 2
Body Section, Body ID 16
XCG: 5.000000 -0.000000 0.500000
AREA: 0.081812
RAD: 0.161374
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
Body Section, Body ID 17
XCG: 6.210307 -0.000000 0.500000
AREA: 0.000818
RAD: 0.016137
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
AwaveTypes: 2 5 4 2 2
Points for all four fuselage sections :: 5 0 0 0
Number of Mach-Alpha cases = 2
Value of CdWave = 1.133328 0.216381
real 0m0.366s
user 0m0.362s
sys 0m0.027s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./awaveTest passed (as expected)
=============================================
=================================================
+ echo './frictionTest test;'
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/cCAPSlog.txt
./frictionTest test;
+ ./frictionTest 0
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/cCAPSlog.txt
Attention: frictionTest is hard coded to look for ../csmData/frictionWingTailFuselage.csm
To not make system calls to the friction executable the second command line option may be supplied - 0 = no analysis , >0 run analysis (default).
Lifting Surface: Body = 1, units m
XLE: 1.571946 -3.872983 0.249728
XTE: 2.536563 -3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 2, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.614012 0.000000 0.002015
Chord: 1.614013
Arc: 3.308635
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 3, units m
XLE: 1.571946 3.872983 0.249728
XTE: 2.536563 3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 4, units m
XLE: 5.484123 0.000000 1.468246
XTE: 6.210307 0.000915 1.468246
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 5, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.210307 0.001525 0.500000
Chord: 1.210308
Arc: 2.471195
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 6, units m
XLE: 5.484123 -0.968246 0.500000
XTE: 6.210307 -0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 7, units m
XLE: 5.484123 0.968246 0.500000
XTE: 6.210307 0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 8, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 9, units m
Arc: 3.714180
Diameter: 1.020621
Type: Fuse
Body of Revolution: Body = 10, units m
Arc: 2.771209
Diameter: 0.645497
Type: Fuse
Body of Revolution: Body = 11, units m
Arc: 1.013945
Diameter: 0.322749
Type: Fuse
Body of Revolution: Body = 12, units m
Arc: 0.101394
Diameter: 0.032275
Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2
Running FRICTION!
Value of CDfric = 0.009900
Value of CDfric = 0.009190
real 0m0.218s
user 0m0.167s
sys 0m0.028s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./frictionTest passed (as expected)
=============================================
All tests pass!
(cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest; ./execute_PyTestRegression.sh LINEARAERO)
=================================================
Using python : /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/venv/bin/python
=================================================
Running.... LINEARAERO PyTests
avl: /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/bin/avl
=================================================
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'avl_PyTest.py test;'
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
CXtot 0.000611907868574681
CYtot -6.289312383470904e-15
CZtot -0.3012861394886091
Cltot -4.782081713039163e-14
Cmtot -0.1945055953450467
Cntot -2.339461801636068e-15
Cl'tot -4.7854363026524e-14
Cn'tot -1.504517153549636e-15
CLtot 0.3012509314150773
CDtot 0.004646353488232845
CDvis 0.0
CLff 0.3009503023520526
CYff -7.719145079534105e-15
CDind 0.004646353488232845
CDff 0.004968969500908293
e 0.9669902146157952
StripForces
Wing cl = [0.02994790451347, 0.08555545178934, 0.1329003532588, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.310122128419, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805665, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996428, 0.2453427152623, 0.2100182422922, 0.1733025192801, 0.1329003532723, 0.08555545180788, 0.0299479045408]
Wing cd = [-0.004234137763162, -0.004494543653191, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946402, 0.0005114598078397, 0.0021191472861, 0.004145189908974, 0.006609094404182, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.00660909440444, 0.004145189909261, 0.002119147286385, 0.0005114598080999, -0.000738653894407, -0.001762021024095, -0.002739626801367, -0.003752887372445, -0.004494543653161, -0.004234137764545]
real 0m0.937s
user 0m0.833s
sys 0m0.386s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'avl_AutoSpan_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
avl_AutoSpan_PyTest.py test;
+ python -u avl_AutoSpan_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wing3, index = 3
Getting vortex lattice surface data
VLM surface name - Wing1
VLM surface name - Wing2
VLM surface name - Wing3
Done getting vortex lattice surface data
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Writing surface - Wing1 (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing surface - Wing2 (ID = 1)
Section 1 of 7 (ID = 0)
Section 2 of 7 (ID = 1)
Section 3 of 7 (ID = 2)
Section 4 of 7 (ID = 3)
Section 5 of 7 (ID = 4)
Section 6 of 7 (ID = 5)
Section 7 of 7 (ID = 6)
Writing surface - Wing3 (ID = 2)
Section 1 of 7 (ID = 0)
Section 2 of 7 (ID = 3)
Control surface 1 of 1
Section 3 of 7 (ID = 4)
Control surface 1 of 1
Section 4 of 7 (ID = 1)
Section 5 of 7 (ID = 5)
Control surface 1 of 1
Section 6 of 7 (ID = 6)
Control surface 1 of 1
Section 7 of 7 (ID = 2)
CXtot -0.04120015166388366
CYtot -3.068870656559766e-11
CZtot -1.125018789839933
Cltot -9.405442101691718e-11
Cmtot -1.954741199601872
Cntot 9.615543347751105e-12
Cl'tot -9.387228170241321e-11
Cn'tot 1.125555483673593e-11
CLtot 1.124128402236974
CDtot 0.06082816185109519
CDvis 0.0
CLff 1.123105423848684
CYff -3.450212807308236e-11
CDind 0.06082816185109519
CDff -0.2032092696193209
e -0.3293035228299759
real 0m16.105s
user 0m19.477s
sys 1m19.943s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case avl_AutoSpan_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'avl_DesignSweep_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
avl_DesignSweep_PyTest.py test;
+ python -u avl_DesignSweep_PyTest.py -outLevel=0 -noPlotData
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002572533601559652
Cl = 0.2009337808878334
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002586364230250732
Cl = 0.2015191856819673
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002609799718825176
Cl = 0.2025075296438165
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002643444008433758
Cl = 0.2039185811663645
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002688200921007501
Cl = 0.20578163777955
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002745342060025447
Cl = 0.2081373840564919
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.00281661033430853
Cl = 0.2110406736710595
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002904376657744787
Cl = 0.2145646488021107
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003011879793053208
Cl = 0.2188068842340149
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003143602034597161
Cl = 0.2238987294821042
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003305877285463858
Cl = 0.2300199286492603
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003507917885484747
Cl = 0.2374223860302241
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003763643677273059
Cl = 0.2464707142750712
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.004095167898241433
Cl = 0.2577158067753745
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.004540047408151035
Cl = 0.2720394012169929
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.005168237926869612
Cl = 0.2909701507469994
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.006128930715349804
Cl = 0.3174875485942861
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.007818359051296945
Cl = 0.3586078919926845
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.01186220444377367
Cl = 0.4382638635253499
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002572533601559652
Cl = 0.2009337808878334
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002586364230250732
Cl = 0.2015191856819673
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002609799718825176
Cl = 0.2025075296438165
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002643444008433758
Cl = 0.2039185811663645
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002688200921007501
Cl = 0.20578163777955
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002745342060025447
Cl = 0.2081373840564919
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.00281661033430853
Cl = 0.2110406736710595
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002904376657744787
Cl = 0.2145646488021107
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003011879793053208
Cl = 0.2188068842340149
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003143602034597161
Cl = 0.2238987294821042
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003305877285463858
Cl = 0.2300199286492603
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003507917885484747
Cl = 0.2374223860302241
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003763643677273059
Cl = 0.2464707142750712
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.004095167898241433
Cl = 0.2577158067753745
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.004540047408151035
Cl = 0.2720394012169929
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.005168237926869612
Cl = 0.2909701507469994
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.006128930715349804
Cl = 0.3174875485942861
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.007818359051296945
Cl = 0.3586078919926845
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.01186220444377367
Cl = 0.4382638635253499
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002572533601559652
Cl = 0.2009337808878334
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002586364230250732
Cl = 0.2015191856819673
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002609799718825176
Cl = 0.2025075296438165
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002643444008433758
Cl = 0.2039185811663645
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002688200921007501
Cl = 0.20578163777955
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002745342060025447
Cl = 0.2081373840564919
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.00281661033430853
Cl = 0.2110406736710595
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002904376657744787
Cl = 0.2145646488021107
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003011879793053208
Cl = 0.2188068842340149
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003143602034597161
Cl = 0.2238987294821042
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003305877285463858
Cl = 0.2300199286492603
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003507917885484747
Cl = 0.2374223860302241
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003763643677273059
Cl = 0.2464707142750712
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.004095167898241433
Cl = 0.2577158067753745
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.004540047408151035
Cl = 0.2720394012169929
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.005168237926869612
Cl = 0.2909701507469994
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.006128930715349804
Cl = 0.3174875485942861
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.007818359051296945
Cl = 0.3586078919926845
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.01186220444377367
Cl = 0.4382638635253499
Cl[0] = 0.2009337808878334
Cd[0] = 0.002572533601559652
real 0m37.111s
user 0m25.528s
sys 0m7.078s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case avl_DesignSweep_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'avl_ControlSurf_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
avl_ControlSurf_PyTest.py test;
+ python -u avl_ControlSurf_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting design parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice control surface data
VLM control surface name - Tail
VLM control surface name - WingRightLE
VLM control surface name - WingRightTE
Done getting vortex lattice control surface data
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Alpha 1.0
Beta 0.0
Mach 0.5
pb/2V -0.0
qc/2V 0.0
rb/2V -0.0
p'b/2V -0.0
r'b/2V -0.0
CXtot -0.01911479917643524
CYtot 0.0382877040111803
CZtot -0.6203123021542292
Cltot 0.05803020542928702
Cmtot -0.3649415791577337
Cntot -0.02051317548234315
Cl'tot 0.05766336287208735
Cn'tot -0.02152281795715037
CLtot 0.6198842263418668
CDtot 0.02993783031517868
CDvis 0.0
CLff 0.6192452092597199
CYff 0.03287079625846207
CDind 0.02993783031517868
CDff 0.02861019822660971
e 0.7130586920545291
real 0m1.369s
user 0m1.042s
sys 0m0.394s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case avl_ControlSurf_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'avl_EigenValue_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
avl_EigenValue_PyTest.py test;
+ python -u avl_EigenValue_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing mass properties file: caps.mass
Parsing MassProp
EigenValues {'case 1': [[0.48252996, 1.0092579], [0.48252996, -1.0092579], [-6.42569, 0.0], [-1.2733929, 0.0], [-0.0011487329, 0.0], [-1.2380479, 0.49321593], [-1.2380479, -0.49321593], [0.77888703, 0.0]]}
real 0m0.783s
user 0m0.558s
sys 0m0.277s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case avl_EigenValue_PyTest.py passed (as expected)
=================================================
=================================================
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'avl_OpenMDAO_3_PyTest.py test;'
avl_OpenMDAO_3_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u avl_OpenMDAO_3_PyTest.py -outLevel=0
[1719109646.383203] [reynolds:1730397:0] ucp_context.c:1774 UCX WARN UCP version is incompatible, required: 1.16, actual: 1.12 (release 1)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Alpha [2.] Beta [3.] Cmtot2 [0.04166298]
Alpha [2.] Beta [3.] Cmtot2 [0.04166298]
Cmtot2_Alpha [[0.68007176]]
Cmtot2_Beta [[0.0008466]]
RUNNING THE L-BFGS-B CODE
* * *
Machine precision = 2.220D-16
N = 2 M = 10
At X0 0 variables are exactly at the bounds
At iterate 0 f= 4.16630D-02 |proj g|= 6.80072D-01
Alpha [1.31992824] Beta [2.9991534] Cmtot2 [0.03401795]
Cmtot2_Alpha [[0.60837327]]
Cmtot2_Beta [[0.0015253]]
At iterate 1 f= 3.40180D-02 |proj g|= 6.08373D-01
Alpha [-4.45133036] Beta [2.92288326] Cmtot2 [0.00071304]
Cmtot2_Alpha [[0.07860089]]
Cmtot2_Beta [[0.00107544]]
At iterate 2 f= 7.13044D-04 |proj g|= 7.86009D-02
Alpha [-5.30773219] Beta [2.90057802] Cmtot2 [2.43104345e-05]
Cmtot2_Alpha [[0.01420175]]
Cmtot2_Beta [[0.00021881]]
At iterate 3 f= 2.43104D-05 |proj g|= 1.42017D-02
Alpha [-5.49659696] Beta [2.89526135] Cmtot2 [3.72334447e-08]
Cmtot2_Alpha [[0.00055304]]
Cmtot2_Beta [[8.7325759e-06]]
At iterate 4 f= 3.72334D-08 |proj g|= 5.53036D-04
Alpha [-5.50424967] Beta [2.89504288] Cmtot2 [2.1976458e-12]
Cmtot2_Alpha [[4.24793145e-06]]
Cmtot2_Beta [[6.71418676e-08]]
At iterate 5 f= 2.19765D-12 |proj g|= 4.24793D-06
* * *
Tit = total number of iterations
Tnf = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip = number of BFGS updates skipped
Nact = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F = final function value
* * *
N Tit Tnf Tnint Skip Nact Projg F
2 5 6 5 0 0 4.248D-06 2.198D-12
F = 2.1976458018921074E-012
CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH
Optimization Complete
-----------------------------------
Optimized values: [-5.50424967] [2.89504288]
real 0m6.246s
user 0m4.268s
sys 0m1.165s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case avl_OpenMDAO_3_PyTest.py passed (as expected)
=================================================
awave: /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/awave
=================================================
+ echo 'awave_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
awave_PyTest.py test;
+ python -u awave_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Writing Awave input file
Body Section, Body ID 1
XCG: 1.571025 -3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :RightWingTank
Awave TYPE: 3
Body Section, Body ID 2
XCG: 2.539271 -3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :RightWingTank
Awave TYPE: 3
Body Section, Body ID 3
XCG: 1.571025 3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :LeftWingTank
Awave TYPE: 3
Body Section, Body ID 4
XCG: 2.539271 3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :LeftWingTank
Awave TYPE: 3
Lifting Surface Section, Body ID 5
XLE: 1.571946 -3.872983 0.249728
CHORD: 0.968408
ATTRIB:Wing
NAME :Wing
Awave TYPE: 0
Lifting Surface Section, Body ID 6
XLE: 0.000000 0.000000 0.000000
CHORD: 1.614013
ATTRIB:Wing
NAME :Wing
Awave TYPE: 1
Lifting Surface Section, Body ID 7
XLE: 1.571946 3.872983 0.249728
CHORD: 0.968408
ATTRIB:Wing
NAME :Wing
Awave TYPE: 1
Lifting Surface Section, Body ID 8
XLE: 5.484123 0.000000 1.468246
CHORD: 0.726185
ATTRIB:VTail
NAME :VertTail
Awave TYPE: 4
Lifting Surface Section, Body ID 9
XLE: 5.000000 0.000000 0.500000
CHORD: 1.210308
ATTRIB:VTail
NAME :VertTail
Awave TYPE: 4
Lifting Surface Section, Body ID 10
XLE: 5.484123 -0.968246 0.500000
CHORD: 0.726185
ATTRIB:HTail
NAME :Stab
Awave TYPE: 0
Lifting Surface Section, Body ID 11
XLE: 5.484123 0.000000 0.500000
CHORD: 0.726185
ATTRIB:HTail
NAME :Stab
Awave TYPE: 5
Lifting Surface Section, Body ID 12
XLE: 5.484123 0.968246 0.500000
CHORD: 0.726185
ATTRIB:HTail
NAME :Stab
Awave TYPE: 5
Body Section, Body ID 13
XCG: -2.000000 0.000000 0.000000
AREA: 0.000000
RAD: 0.000000
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
Body Section, Body ID 14
XCG: 0.000000 -0.000000 -0.000000
AREA: 0.818123
RAD: 0.510310
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
Warning: capsGroup not found on body 15!
Body Section, Body ID 15
XCG: 1.613743 -0.000000 0.000000
AREA: 0.327249
RAD: 0.322749
ATTRIB:Fuse
NAME :(null)
Awave TYPE: 2
Body Section, Body ID 16
XCG: 5.000000 -0.000000 0.500000
AREA: 0.081812
RAD: 0.161374
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
Body Section, Body ID 17
XCG: 6.210307 -0.000000 0.500000
AREA: 0.000818
RAD: 0.016137
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
AwaveTypes: 2 5 4 2 2
Points for all four fuselage sections :: 5 0 0 0
Number of Mach-Alpha cases = 2
CdWave = [1.13332772, 0.216380954]
real 0m0.650s
user 0m0.628s
sys 0m0.304s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case awave_PyTest.py passed (as expected)
=================================================
friction: /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/friction
=================================================
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'friction_PyTest.py test;'
friction_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u friction_PyTest.py -outLevel=0
Loading AIM
Setting Mach & Altitude Values
Lifting Surface: Body = 1, units m
XLE: 1.571946 -3.872983 0.249728
XTE: 2.536563 -3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 2, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.614012 0.000000 0.002015
Chord: 1.614013
Arc: 3.308635
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 3, units m
XLE: 1.571946 3.872983 0.249728
XTE: 2.536563 3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 4, units m
XLE: 5.484123 0.000000 1.468246
XTE: 6.210307 0.000915 1.468246
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 5, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.210307 0.001525 0.500000
Chord: 1.210308
Arc: 2.471195
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 6, units m
XLE: 5.484123 -0.968246 0.500000
XTE: 6.210307 -0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 7, units m
XLE: 5.484123 0.968246 0.500000
XTE: 6.210307 0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 8, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 9, units m
Arc: 3.714180
Diameter: 1.020621
Type: Fuse
Body of Revolution: Body = 10, units m
Arc: 2.771209
Diameter: 0.645497
Type: Fuse
Body of Revolution: Body = 11, units m
Arc: 1.013945
Diameter: 0.322749
Type: Fuse
Body of Revolution: Body = 12, units m
Arc: 0.101394
Diameter: 0.032275
Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2
Total drag = [0.0132, 0.01226]
Form drag = [0.0033, 0.00307]
Friction drag = [0.0099, 0.00919]
real 0m0.584s
user 0m0.476s
sys 0m0.293s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected)
=================================================
tsfoil2: /home/jenkins/util/tsfoil/tsfoil2
=================================================
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'tsfoil_PyTest.py test;'
tsfoil_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u tsfoil_PyTest.py -outLevel=0
Getting results
PAUSE Press the ENTER key to exit
To resume execution, type go. Other input will terminate the job.
Note: The following floating-point exceptions are signalling: IEEE_OVERFLOW_FLAG IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Cl = 0.933329
Cd = 0.000283
Cd Wave = 0.0
Cm = -0.203433
Cp _Critcal = -1.303869
real 0m0.521s
user 0m0.477s
sys 0m0.186s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected)
=================================================
mses: /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/bin/mses
=================================================
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'mses_PyTest.py test;'
mses_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
Cl = 0.37837910855492335
Cd = 0.00777585841721013
Cm = 0.0052626369958117215
real 0m6.665s
user 0m6.259s
sys 0m0.370s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected)
=================================================
=================================================
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'mses_OpenMDAO_3_PyTest.py test;'
mses_OpenMDAO_3_PyTest.py test;
+ python -u mses_OpenMDAO_3_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
[1719109661.333215] [reynolds:1745915:0] ucp_context.c:1774 UCX WARN UCP version is incompatible, required: 1.16, actual: 1.12 (release 1)
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - camber
Done getting CFD design variables
camber [0.1] CD [0.01326534]
camber [0.1] CD [0.01326534]
CD_camber [[0.1764758]]
RUNNING THE L-BFGS-B CODE
* * *
Machine precision = 2.220D-16
N = 1 M = 10
At X0 1 variables are exactly at the bounds
At iterate 0 f= 1.32653D-02 |proj g|= 1.76476D-01
camber [-0.0764758] CD [0.01022332]
CD_camber [[-0.08759845]]
At iterate 1 f= 1.02233D-02 |proj g|= 8.75985D-02
camber [-0.01793542] CD [0.00770373]
CD_camber [[-0.01328901]]
At iterate 2 f= 7.70373D-03 |proj g|= 1.32890D-02
camber [-0.00746645] CD [0.00760241]
CD_camber [[-0.00542413]]
At iterate 3 f= 7.60241D-03 |proj g|= 5.42413D-03
camber [-0.00024637] CD [0.00758207]
CD_camber [[-0.00011784]]
At iterate 4 f= 7.58207D-03 |proj g|= 1.17837D-04
camber [-8.60314e-05] CD [0.00758208]
CD_camber [[-3.33327477e-06]]
camber [-0.00022179] CD [0.00758207]
CD_camber [[-0.00010258]]
camber [-0.00024453] CD [0.00758207]
CD_camber [[-0.00011643]]
camber [-0.00024634] CD [0.00758207]
CD_camber [[-0.00011757]]
camber [-0.00024637] CD [0.00758207]
CD_camber [[-0.00011784]]
camber [-0.00024637] CD [0.00758207]
CD_camber [[-0.00011784]]
camber [-0.00024637] CD [0.00758207]
CD_camber [[-0.00011784]]
camber [-0.00024637] CD [0.00758207]
CD_camber [[-0.00011784]]
camber [-0.00024637] CD [0.00758207]
CD_camber [[-0.00011784]]
camber [-0.00024637] CD [0.00758207]
CD_camber [[-0.00011784]]
camber [-0.00024637] CD [0.00758207]
CD_camber [[-0.00011784]]
camber [-0.00024637] CD [0.00758207]
CD_camber [[-0.00011784]]
camber [-0.00024637] CD [0.00758207]
CD_camber [[-0.00011784]]
camber [-0.00024637] CD [0.00758207]
CD_camber [[-0.00011784]]
At iterate 5 f= 7.58207D-03 |proj g|= 1.17837D-04
* * *
Tit = total number of iterations
Tnf = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip = number of BFGS updates skipped
Nact = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F = final function value
* * *
N Tit Tnf Tnint Skip Nact Projg F
1 5 22 5 0 0 1.178D-04 7.582D-03
F = 7.5820673299879966E-003
CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH
Warning: more than 10 function and gradient
evaluations in the last line search. Termination
may possibly be caused by a bad search direction.
Optimization Complete
-----------------------------------
Optimized values: [-0.00024637]
real 2m34.699s
user 2m16.116s
sys 0m2.796s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case mses_OpenMDAO_3_PyTest.py passed (as expected)
=================================================
xfoil: /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/bin/xfoil
=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Cl = [1.05475230552212, 1.36488869373643, 1.56607214272092, 2.03059709361332, 1.97271083121472, 1.87307153172173, 1.7605047576014]
Cd = [0.0131991208675769, 0.016654024060569, 0.0200551482562873, 0.0458671341846591, 0.07542560093919, 0.0994469174479714, 0.127479430988999]
Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0]
Transition location = [0.496044114214226, 0.461377732041584, 0.442376568201776, 0.361251636069055, 0.276104140854801, 0.214381239320269, 0.132988264746769]
real 0m11.528s
user 0m8.145s
sys 0m0.397s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected)
=================================================
awave: /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/test/awave
=================================================
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'autoLink_Pytest.py test;'
autoLink_Pytest.py test;
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u autoLink_Pytest.py -outLevel=0 -noPlotData
Linked Parameter Mach to analysis friction input Mach
Linked Parameter Mach to analysis awave input Mach
Linked Parameter Mach to analysis avl input Mach
Linked Parameter Alpha to analysis awave input Alpha
Linked Parameter Alpha to analysis avl input Alpha
Linked Parameter Altitude to analysis friction input Altitude
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = RightTank, index = 1
Name = LeftTank, index = 2
Name = Wing, index = 3
Name = VertTail, index = 4
Name = HorizTail, index = 5
Name = Fuselage, index = 6
Getting vortex lattice surface data
VLM surface name - HorizTail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - VertTail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Warning (vlm_getSections): No capsGroup value found on body 15, body will not be used
Warning (vlm_getSections): No capsGroup value found on body 15, body will not be used
Warning (vlm_getSections): No capsGroup value found on body 15, body will not be used
Writing surface - HorizTail (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing surface - VertTail (ID = 1)
Section 1 of 2 (ID = 0)
Section 2 of 2 (ID = 1)
Writing surface - Wing (ID = 2)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Cd = [[0.01954019062669618, 0.017418911634865274, 0.016377545441610297, 0.015723407368881608, 0.01529976634123673, 0.01505125860577304, 0.014977771651912518], [0.020030190626696177, 0.017828911634865274, 0.016737545441610296, 0.016063407368881608, 0.01561976634123673, 0.01535125860577304, 0.015267771651912518], [0.020570190626696176, 0.018268911634865274, 0.017127545441610298, 0.016423407368881607, 0.015949766341236727, 0.01567125860577304, 0.015577771651912518], [0.021140190626696177, 0.018738911634865272, 0.017547545441610298, 0.016813407368881608, 0.01631976634123673, 0.01601125860577304, 0.015907771651912518], [0.021770190626696176, 0.019248911634865272, 0.018007545441610297, 0.01723340736888161, 0.01671976634123673, 0.016391258605773038, 0.016267771651912517], [0.02246019062669618, 0.019808911634865273, 0.018507545441610297, 0.017693407368881607, 0.017139766341236727, 0.01680125860577304, 0.016657771651912515], [0.02321019062669618, 0.020418911634865273, 0.019047545441610296, 0.018193407368881608, 0.01760976634123673, 0.017241258605773038, 0.017077771651912516], [0.02425019062669618, 0.021258911634865273, 0.019797545441610297, 0.018873407368881608, 0.01824976634123673, 0.01785125860577304, 0.017657771651912516], [0.02543019062669618, 0.022218911634865272, 0.020637545441610297, 0.01965340736888161, 0.01897976634123673, 0.018531258605773038, 0.018307771651912517], [0.026710190626696176, 0.023248911634865272, 0.021547545441610298, 0.020483407368881608, 0.019759766341236728, 0.01927125860577304, 0.019007771651912517], [0.028100190626696178, 0.024358911634865272, 0.022527545441610296, 0.021383407368881606, 0.02058976634123673, 0.020061258605773038, 0.019757771651912517], [0.029590190626696176, 0.025548911634865272, 0.023577545441610295, 0.022333407368881612, 0.02148976634123673, 0.02090125860577304, 0.020557771651912516]]
real 1m40.553s
user 1m27.091s
sys 0m8.042s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case autoLink_Pytest.py passed (as expected)
=================================================
*************************************************
*************************************************
All tests pass!
++ cd /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest
++ ./execute_PyTestRegression.sh LINEARAERO
=================================================
Legacy Using python : /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/ESP/venv/bin/python
=================================================
Running.... LINEARAERO PyTests
=================================================
+ rm -rf avl_PyTest
+ echo 'avl_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Running AVL
CXtot 0.000611907868574681
CYtot -6.289312383470904e-15
CZtot -0.3012861394886091
Cltot -4.782081713039163e-14
Cmtot -0.1945055953450467
Cntot -2.339461801636068e-15
Cl'tot -4.7854363026524e-14
Cn'tot -1.504517153549636e-15
CLtot 0.3012509314150773
CDtot 0.004646353488232845
CDvis 0.0
CLff 0.3009503023520526
CYff -7.719145079534105e-15
CDind 0.004646353488232845
CDff 0.004968969500908293
e 0.9669902146157952
StripForces
Wing cl = [0.02994790451347, 0.08555545178934, 0.1329003532588, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.310122128419, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805665, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996428, 0.2453427152623, 0.2100182422922, 0.1733025192801, 0.1329003532723, 0.08555545180788, 0.0299479045408]
Wing cd = [-0.004234137763162, -0.004494543653191, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946402, 0.0005114598078397, 0.0021191472861, 0.004145189908974, 0.006609094404182, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.00660909440444, 0.004145189909261, 0.002119147286385, 0.0005114598080999, -0.000738653894407, -0.001762021024095, -0.002739626801367, -0.003752887372445, -0.004494543653161, -0.004234137764545]
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
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.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m0.830s
user 0m0.698s
sys 0m0.449s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf avl_AutoSpan_PyTest
+ echo 'avl_AutoSpan_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
avl_AutoSpan_PyTest.py test;
+ python -u avl_AutoSpan_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wing3, index = 3
Getting vortex lattice surface data
VLM surface name - Wing1
VLM surface name - Wing2
VLM surface name - Wing3
Done getting vortex lattice surface data
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Writing surface - Wing1 (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing surface - Wing2 (ID = 1)
Section 1 of 7 (ID = 0)
Section 2 of 7 (ID = 1)
Section 3 of 7 (ID = 2)
Section 4 of 7 (ID = 3)
Section 5 of 7 (ID = 4)
Section 6 of 7 (ID = 5)
Section 7 of 7 (ID = 6)
Writing surface - Wing3 (ID = 2)
Section 1 of 7 (ID = 0)
Section 2 of 7 (ID = 3)
Control surface 1 of 1
Section 3 of 7 (ID = 4)
Control surface 1 of 1
Section 4 of 7 (ID = 1)
Section 5 of 7 (ID = 5)
Control surface 1 of 1
Section 6 of 7 (ID = 6)
Control surface 1 of 1
Section 7 of 7 (ID = 2)
Running AVL
CXtot -0.03128890105580789
CYtot -2.110424606000471e-11
CZtot -1.01466313745144
Cltot -6.716893701126918e-11
Cmtot -2.941985138524287
Cntot 8.039793668222176e-12
Cl'tot -6.70183931100526e-11
Cn'tot 9.210828757385857e-12
CLtot 1.013962532722773
CDtot 0.04899244907635769
CDvis 0.0
CLff 1.012753587462204
CYff -2.520302490874793e-11
CDind 0.04899244907635769
CDff -0.08941639978555985
e -0.6085401584783248
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m20.094s
user 0m21.018s
sys 0m18.979s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case avl_AutoSpan_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf avl_DesignSweep_PyTest
+ echo 'avl_DesignSweep_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
avl_DesignSweep_PyTest.py test;
+ python -u avl_DesignSweep_PyTest.py -verbosity=0 -workDir=runDirectory -noPlotData
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 5) at Mach number = 0.05!
Cd = 0.002572533601559652
Cl = 0.2009337808878334
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 5) at Mach number = 0.1!
Cd = 0.002586364230250732
Cl = 0.2015191856819673
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 5) at Mach number = 0.15000000000000002!
Cd = 0.002609799718825176
Cl = 0.2025075296438165
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 5) at Mach number = 0.2!
Cd = 0.002643444008433758
Cl = 0.2039185811663645
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 5) at Mach number = 0.25!
Cd = 0.002688200921007501
Cl = 0.20578163777955
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 5) at Mach number = 0.30000000000000004!
Cd = 0.002745342060025447
Cl = 0.2081373840564919
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 5) at Mach number = 0.35000000000000003!
Cd = 0.00281661033430853
Cl = 0.2110406736710595
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 5) at Mach number = 0.4!
Cd = 0.002904376657744787
Cl = 0.2145646488021107
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 5) at Mach number = 0.45!
Cd = 0.003011879793053208
Cl = 0.2188068842340149
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 5) at Mach number = 0.5!
Cd = 0.003143602034597161
Cl = 0.2238987294821042
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 5) at Mach number = 0.55!
Cd = 0.003305877285463858
Cl = 0.2300199286492603
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 5) at Mach number = 0.6000000000000001!
Cd = 0.003507917885484747
Cl = 0.2374223860302241
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 5) at Mach number = 0.65!
Cd = 0.003763643677273059
Cl = 0.2464707142750712
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 5) at Mach number = 0.7000000000000001!
Cd = 0.004095167898241433
Cl = 0.2577158067753745
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 5) at Mach number = 0.75!
Cd = 0.004540047408151035
Cl = 0.2720394012169929
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 5) at Mach number = 0.8!
Cd = 0.005168237926869612
Cl = 0.2909701507469994
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 5) at Mach number = 0.8500000000000001!
Cd = 0.006128930715349804
Cl = 0.3174875485942861
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 5) at Mach number = 0.9!
Cd = 0.007818359051296945
Cl = 0.3586078919926845
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 5) at Mach number = 0.9500000000000001!
Cd = 0.01186220444377367
Cl = 0.4382638635253499
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 10) at Mach number = 0.05!
Cd = 0.002572533601559652
Cl = 0.2009337808878334
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 10) at Mach number = 0.1!
Cd = 0.002586364230250732
Cl = 0.2015191856819673
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 10) at Mach number = 0.15000000000000002!
Cd = 0.002609799718825176
Cl = 0.2025075296438165
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 10) at Mach number = 0.2!
Cd = 0.002643444008433758
Cl = 0.2039185811663645
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 10) at Mach number = 0.25!
Cd = 0.002688200921007501
Cl = 0.20578163777955
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 10) at Mach number = 0.30000000000000004!
Cd = 0.002745342060025447
Cl = 0.2081373840564919
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 10) at Mach number = 0.35000000000000003!
Cd = 0.00281661033430853
Cl = 0.2110406736710595
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 10) at Mach number = 0.4!
Cd = 0.002904376657744787
Cl = 0.2145646488021107
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 10) at Mach number = 0.45!
Cd = 0.003011879793053208
Cl = 0.2188068842340149
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 10) at Mach number = 0.5!
Cd = 0.003143602034597161
Cl = 0.2238987294821042
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 10) at Mach number = 0.55!
Cd = 0.003305877285463858
Cl = 0.2300199286492603
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 10) at Mach number = 0.6000000000000001!
Cd = 0.003507917885484747
Cl = 0.2374223860302241
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 10) at Mach number = 0.65!
Cd = 0.003763643677273059
Cl = 0.2464707142750712
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 10) at Mach number = 0.7000000000000001!
Cd = 0.004095167898241433
Cl = 0.2577158067753745
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 10) at Mach number = 0.75!
Cd = 0.004540047408151035
Cl = 0.2720394012169929
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 10) at Mach number = 0.8!
Cd = 0.005168237926869612
Cl = 0.2909701507469994
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 10) at Mach number = 0.8500000000000001!
Cd = 0.006128930715349804
Cl = 0.3174875485942861
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 10) at Mach number = 0.9!
Cd = 0.007818359051296945
Cl = 0.3586078919926845
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 10) at Mach number = 0.9500000000000001!
Cd = 0.01186220444377367
Cl = 0.4382638635253499
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 20) at Mach number = 0.05!
Cd = 0.002572533601559652
Cl = 0.2009337808878334
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 20) at Mach number = 0.1!
Cd = 0.002586364230250732
Cl = 0.2015191856819673
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 20) at Mach number = 0.15000000000000002!
Cd = 0.002609799718825176
Cl = 0.2025075296438165
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 20) at Mach number = 0.2!
Cd = 0.002643444008433758
Cl = 0.2039185811663645
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 20) at Mach number = 0.25!
Cd = 0.002688200921007501
Cl = 0.20578163777955
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 20) at Mach number = 0.30000000000000004!
Cd = 0.002745342060025447
Cl = 0.2081373840564919
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 20) at Mach number = 0.35000000000000003!
Cd = 0.00281661033430853
Cl = 0.2110406736710595
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 20) at Mach number = 0.4!
Cd = 0.002904376657744787
Cl = 0.2145646488021107
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 20) at Mach number = 0.45!
Cd = 0.003011879793053208
Cl = 0.2188068842340149
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 20) at Mach number = 0.5!
Cd = 0.003143602034597161
Cl = 0.2238987294821042
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 20) at Mach number = 0.55!
Cd = 0.003305877285463858
Cl = 0.2300199286492603
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 20) at Mach number = 0.6000000000000001!
Cd = 0.003507917885484747
Cl = 0.2374223860302241
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 20) at Mach number = 0.65!
Cd = 0.003763643677273059
Cl = 0.2464707142750712
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 20) at Mach number = 0.7000000000000001!
Cd = 0.004095167898241433
Cl = 0.2577158067753745
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 20) at Mach number = 0.75!
Cd = 0.004540047408151035
Cl = 0.2720394012169929
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 20) at Mach number = 0.8!
Cd = 0.005168237926869612
Cl = 0.2909701507469994
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 20) at Mach number = 0.8500000000000001!
Cd = 0.006128930715349804
Cl = 0.3174875485942861
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 20) at Mach number = 0.9!
Cd = 0.007818359051296945
Cl = 0.3586078919926845
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL (sweep angle = 20) at Mach number = 0.9500000000000001!
Cd = 0.01186220444377367
Cl = 0.4382638635253499
Cl[0] = 0.2009337808878334
Cd[0] = 0.002572533601559652
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
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.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m43.286s
user 0m30.772s
sys 0m7.771s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case avl_DesignSweep_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf avl_ControlSurf_PyTest
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
+ echo 'avl_ControlSurf_PyTest.py test;'
avl_ControlSurf_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
+ python -u avl_ControlSurf_PyTest.py -verbosity=0 -workDir=runDirectory
Loading AIM
Setting design parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice control surface data
VLM control surface name - Tail
VLM control surface name - WingRightLE
VLM control surface name - WingRightTE
Done getting vortex lattice control surface data
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Running AVL
Alpha 1.0
Beta 0.0
Mach 0.5
pb/2V -0.0
qc/2V 0.0
rb/2V -0.0
p'b/2V -0.0
r'b/2V -0.0
CXtot -0.01911479917643524
CYtot 0.0382877040111803
CZtot -0.6203123021542292
Cltot 0.05803020542928702
Cmtot -0.3649415791577337
Cntot -0.02051317548234315
Cl'tot 0.05766336287208735
Cn'tot -0.02152281795715037
CLtot 0.6198842263418668
CDtot 0.02993783031517868
CDvis 0.0
CLff 0.6192452092597199
CYff 0.03287079625846207
CDind 0.02993783031517868
CDff 0.02861019822660971
e 0.7130586920545291
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
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.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m1.243s
user 0m1.025s
sys 0m0.424s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case avl_ControlSurf_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf avl_EigenValue_PyTest
+ echo 'avl_EigenValue_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
avl_EigenValue_PyTest.py test;
+ python -u avl_EigenValue_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing mass properties file: caps.mass
Parsing MassProp
Running AVL
EigenValues ('case 1', [[0.48252996, 1.0092579], [0.48252996, -1.0092579], [-6.42569, 0.0], [-1.2733929, 0.0], [-0.0011487329, 0.0], [-1.2380479, 0.49321593], [-1.2380479, -0.49321593], [0.77888703, 0.0]])
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
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.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m1.107s
user 0m0.767s
sys 0m0.416s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case avl_EigenValue_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf awave_PyTest
+ echo 'awave_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
awave_PyTest.py test;
+ python -u awave_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Writing Awave input file
Body Section, Body ID 1
XCG: 1.571025 -3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :RightWingTank
Awave TYPE: 3
Body Section, Body ID 2
XCG: 2.539271 -3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :RightWingTank
Awave TYPE: 3
Body Section, Body ID 3
XCG: 1.571025 3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :LeftWingTank
Awave TYPE: 3
Body Section, Body ID 4
XCG: 2.539271 3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :LeftWingTank
Awave TYPE: 3
Lifting Surface Section, Body ID 5
XLE: 1.571946 -3.872983 0.249728
CHORD: 0.968408
ATTRIB:Wing
NAME :Wing
Awave TYPE: 0
Lifting Surface Section, Body ID 6
XLE: 0.000000 0.000000 0.000000
CHORD: 1.614013
ATTRIB:Wing
NAME :Wing
Awave TYPE: 1
Lifting Surface Section, Body ID 7
XLE: 1.571946 3.872983 0.249728
CHORD: 0.968408
ATTRIB:Wing
NAME :Wing
Awave TYPE: 1
Lifting Surface Section, Body ID 8
XLE: 5.484123 0.000000 1.468246
CHORD: 0.726185
ATTRIB:VTail
NAME :VertTail
Awave TYPE: 4
Lifting Surface Section, Body ID 9
XLE: 5.000000 0.000000 0.500000
CHORD: 1.210308
ATTRIB:VTail
NAME :VertTail
Awave TYPE: 4
Lifting Surface Section, Body ID 10
XLE: 5.484123 -0.968246 0.500000
CHORD: 0.726185
ATTRIB:HTail
NAME :Stab
Awave TYPE: 0
Lifting Surface Section, Body ID 11
XLE: 5.484123 0.000000 0.500000
CHORD: 0.726185
ATTRIB:HTail
NAME :Stab
Awave TYPE: 5
Lifting Surface Section, Body ID 12
XLE: 5.484123 0.968246 0.500000
CHORD: 0.726185
ATTRIB:HTail
NAME :Stab
Awave TYPE: 5
Body Section, Body ID 13
XCG: -2.000000 0.000000 0.000000
AREA: 0.000000
RAD: 0.000000
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
Body Section, Body ID 14
XCG: 0.000000 -0.000000 -0.000000
AREA: 0.818123
RAD: 0.510310
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
Warning: capsGroup not found on body 15!
Body Section, Body ID 15
XCG: 1.613743 -0.000000 0.000000
AREA: 0.327249
RAD: 0.322749
ATTRIB:Fuse
NAME :(null)
Awave TYPE: 2
Body Section, Body ID 16
XCG: 5.000000 -0.000000 0.500000
AREA: 0.081812
RAD: 0.161374
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
Body Section, Body ID 17
XCG: 6.210307 -0.000000 0.500000
AREA: 0.000818
RAD: 0.016137
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
AwaveTypes: 2 5 4 2 2
Points for all four fuselage sections :: 5 0 0 0
Number of Mach-Alpha cases = 2
Running AWAVE
Running Post Analysis
CdWave = [1.13332772, 0.216380954]
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m0.854s
user 0m0.737s
sys 0m0.132s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case awave_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf friction_PyTest
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
+ echo 'friction_PyTest.py test;'
friction_PyTest.py test;
+ python -u friction_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting Mach & Altitude Values
Lifting Surface: Body = 1, units m
XLE: 1.571946 -3.872983 0.249728
XTE: 2.536563 -3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 2, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.614012 0.000000 0.002015
Chord: 1.614013
Arc: 3.308635
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 3, units m
XLE: 1.571946 3.872983 0.249728
XTE: 2.536563 3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 4, units m
XLE: 5.484123 0.000000 1.468246
XTE: 6.210307 0.000915 1.468246
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 5, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.210307 0.001525 0.500000
Chord: 1.210308
Arc: 2.471195
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 6, units m
XLE: 5.484123 -0.968246 0.500000
XTE: 6.210307 -0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 7, units m
XLE: 5.484123 0.968246 0.500000
XTE: 6.210307 0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 8, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 9, units m
Arc: 3.714180
Diameter: 1.020621
Type: Fuse
Body of Revolution: Body = 10, units m
Arc: 2.771209
Diameter: 0.645497
Type: Fuse
Body of Revolution: Body = 11, units m
Arc: 1.013945
Diameter: 0.322749
Type: Fuse
Body of Revolution: Body = 12, units m
Arc: 0.101394
Diameter: 0.032275
Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2
Total drag = [0.0132, 0.01226]
Form drag = [0.0033, 0.00307]
Friction drag = [0.0099, 0.00919]
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m0.722s
user 0m0.561s
sys 0m0.242s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf tsfoil_PyTest
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
+ echo 'tsfoil_PyTest.py test;'
tsfoil_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
+ python -u tsfoil_PyTest.py -verbosity=0 -workDir=runDirectory
Running tsFoil......
PAUSE Press the ENTER key to exit
To resume execution, type go. Other input will terminate the job.
Note: The following floating-point exceptions are signalling: IEEE_OVERFLOW_FLAG IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Getting results
Cl = 0.933329
Cd = 0.000283
Cd Wave = 0.0
Cm = -0.203433
Cp _Critcal = -1.303869
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m0.683s
user 0m0.555s
sys 0m0.259s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf xfoil_PyTest
+ echo 'xfoil_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -verbosity=0 -workDir=runDirectory -noPlotData
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Running xFoil......
Cl = [1.05475230552212, 1.36488869373643, 1.56607214272092, 2.03059709361332, 1.97271083121472, 1.87307153172173, 1.7605047576014]
Cd = [0.0131991208675769, 0.016654024060569, 0.0200551482562873, 0.0458671341846591, 0.07542560093919, 0.0994469174479714, 0.127479430988999]
Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0]
Transition location = [0.496044114214226, 0.461377732041584, 0.442376568201776, 0.361251636069055, 0.276104140854801, 0.214381239320269, 0.132988264746769]
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m8.930s
user 0m8.019s
sys 0m0.281s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf autoLink_Pytest
+ echo 'autoLink_Pytest.py test;'
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
autoLink_Pytest.py test;
+ python -u autoLink_Pytest.py -verbosity=0 -workDir=runDirectory -noPlotData
+ tee -a /jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Linked Parameter Mach to analysis frictionAIM input Mach
Linked Parameter Mach to analysis awaveAIM input Mach
Linked Parameter Mach to analysis avlAIM input Mach
Linked Parameter Alpha to analysis awaveAIM input Alpha
Linked Parameter Alpha to analysis avlAIM input Alpha
Linked Parameter Altitude to analysis frictionAIM input Altitude
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = RightTank, index = 1
Name = LeftTank, index = 2
Name = Wing, index = 3
Name = VertTail, index = 4
Name = HorizTail, index = 5
Name = Fuselage, index = 6
Getting vortex lattice surface data
VLM surface name - HorizTail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - VertTail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Warning (vlm_getSections): No capsGroup value found on body 15, body will not be used
Warning (vlm_getSections): No capsGroup value found on body 15, body will not be used
Warning (vlm_getSections): No capsGroup value found on body 15, body will not be used
Writing surface - HorizTail (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing surface - VertTail (ID = 1)
Section 1 of 2 (ID = 0)
Section 2 of 2 (ID = 1)
Writing surface - Wing (ID = 2)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 2, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 3, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Body of Revolution: Body = 4, units m
Arc: 0.526861
Diameter: 0.167705
Type: Store
Lifting Surface: Body = 5, units m
XLE: 1.361345 -3.354102 0.216271
XTE: 2.196728 -3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 6, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.397775 0.000000 0.001745
Chord: 1.397776
Arc: 2.865362
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 7, units m
XLE: 1.361345 3.354102 0.216271
XTE: 2.196728 3.354102 0.290409
Chord: 0.838666
Arc: 1.719217
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 8, units m
XLE: 5.419263 0.000000 1.338525
XTE: 6.048157 0.000792 1.338525
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 9, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.048157 0.001321 0.500000
Chord: 1.048158
Arc: 2.140118
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 10, units m
XLE: 5.419263 -0.838525 0.500000
XTE: 6.048157 -0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 11, units m
XLE: 5.419263 0.000000 0.500000
XTE: 6.048157 0.000000 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 12, units m
XLE: 5.419263 0.838525 0.500000
XTE: 6.048157 0.838525 0.500792
Chord: 0.628895
Arc: 1.284071
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 13, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 14, units m
Arc: 3.216574
Diameter: 0.883883
Type: Fuse
Body of Revolution: Body = 15, units m
Arc: 2.399938
Diameter: 0.559017
Type: Fuse
Body of Revolution: Body = 16, units m
Arc: 0.878102
Diameter: 0.279508
Type: Fuse
Body of Revolution: Body = 17, units m
Arc: 0.087810
Diameter: 0.027951
Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Cd = [[0.01954019062669618, 0.017418911634865274, 0.016377545441610297, 0.015723407368881608, 0.01529976634123673, 0.01505125860577304, 0.014977771651912518], [0.020030190626696177, 0.017828911634865274, 0.016737545441610296, 0.016063407368881608, 0.01561976634123673, 0.01535125860577304, 0.015267771651912518], [0.020570190626696176, 0.018268911634865274, 0.017127545441610298, 0.016423407368881607, 0.015949766341236727, 0.01567125860577304, 0.015577771651912518], [0.021140190626696177, 0.018738911634865272, 0.017547545441610298, 0.016813407368881608, 0.01631976634123673, 0.01601125860577304, 0.015907771651912518], [0.021770190626696176, 0.019248911634865272, 0.018007545441610297, 0.01723340736888161, 0.01671976634123673, 0.016391258605773038, 0.016267771651912517], [0.02246019062669618, 0.019808911634865273, 0.018507545441610297, 0.017693407368881607, 0.017139766341236727, 0.01680125860577304, 0.016657771651912515], [0.02321019062669618, 0.020418911634865273, 0.019047545441610296, 0.018193407368881608, 0.01760976634123673, 0.017241258605773038, 0.017077771651912516], [0.02425019062669618, 0.021258911634865273, 0.019797545441610297, 0.018873407368881608, 0.01824976634123673, 0.01785125860577304, 0.017657771651912516], [0.02543019062669618, 0.022218911634865272, 0.020637545441610297, 0.01965340736888161, 0.01897976634123673, 0.018531258605773038, 0.018307771651912517], [0.026710190626696176, 0.023248911634865272, 0.021547545441610298, 0.020483407368881608, 0.019759766341236728, 0.01927125860577304, 0.019007771651912517], [0.028100190626696178, 0.024358911634865272, 0.022527545441610296, 0.021383407368881606, 0.02058976634123673, 0.020061258605773038, 0.019757771651912517], [0.029590190626696176, 0.025548911634865272, 0.023577545441610295, 0.022333407368881612, 0.02148976634123673, 0.02090125860577304, 0.020557771651912516]]
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.setVerbosity' is deprecated. Please use 'Problem.setOutLevel'!
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.addAttribute' is deprecated. Please use 'Analysis.attr.create'!
WARNING: 'capsProblem.createValue' is deprecated. Please use 'Problem.parameter.create'!
WARNING: '_capsValue.__init__' is deprecated. Please use 'Problem.parameter.create'!
WARNING: 'capsProblem.autoLinkValue' is deprecated. Please use 'Problem.autoLinkParameter'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsAnalysis.getAttributeVal' is deprecated. Please use 'Analysis.geometry.attrList'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.aimName' is deprecated. Please use 'name'!
WARNING: 'capsAnalysis.getAttribute' is deprecated. Please use 'Analysis.attr["name"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 1m34.331s
user 1m19.466s
sys 0m9.096s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case autoLink_Pytest.py passed (as expected)
=================================================
*************************************************
*************************************************
All tests pass!
[Execution node] check if [reynolds] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/LINUX64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_RegCaps/CASREV=7.8,ESPTEST=CAPS/LINEARAERO,ESP_ARCH=LINUX64,buildnode=reynolds #665'.
[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